FCC Web Documents citing 25.280
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-1492A1.doc http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-1492A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-1492A1.txt
- as much as six degrees. This inclination would decrease under the influence of gravitational forces of the sun and moon and then would begin to increase, thereby fluctuating between about zero and six degrees during the expected life of the satellite. MSV states that its satellite will operate consistent with the requirements for inclined orbit satellites set forth in Section 25.280 of the Commission's rules. We grant MSV's request. We note, however, that granting this request creates a potential for harmful interference between MSV-1's Ku-band operations and Ku-band NGSO fixed-satellite service (FSS) satellites. Pursuant to ITU Radio Regulations, GSO satellites such as MSV-1 are protected against interference from NGSO FSS satellites operating in the same band, provided that the GSO satellite's
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-1492A1_Erratum.doc
- as much as six degrees. This inclination would decrease under the influence of gravitational forces of the sun and moon and then would begin to increase, thereby fluctuating between about zero and six degrees during the expected life of the satellite. MSV states that its satellite will operate consistent with the requirements for inclined orbit satellites set forth in Section 25.280 of the Commission's rules. We grant MSV's request. We note, however, that granting this request creates a potential for harmful interference between MSV-1's Ku-band operations and Ku-band NGSO fixed-satellite service (FSS) satellites. Pursuant to ITU Radio Regulations, GSO satellites such as MSV-1 are protected against interference from NGSO FSS satellites operating in the same band, provided that the GSO satellite's
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-1504A1.doc http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-1504A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-1504A1.txt
- north-south inclination of as much as six degrees. The inclination would initially decrease under the influence of gravitational forces of the sun and moon and would gradually fluctuate between about zero and six degrees during the expected service lifetime of the satellite. ICO states that its satellite will operate in compliance with the requirements for inclined orbit satellites in Section 25.280 of the Commission's rules. This proposal does not present any cause for concern. We remind ICO, however, that under the ITU Radio Regulations, operation of a GSO satellite in an allocated FSS band is entitled to protection against interference from co-frequency NGSO satellites only if the GSO satellite's north-south inclination is 4.5º or less. Thus, during periods in which ICO-G
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-1504A1_Erratum.doc
- north-south inclination of as much as six degrees. The inclination would initially decrease under the influence of gravitational forces of the sun and moon and would gradually fluctuate between about zero and six degrees during the expected service lifetime of the satellite. ICO states that its satellite will operate in compliance with the requirements for inclined orbit satellites in Section 25.280 of the Commission's rules. This proposal does not present any cause for concern. We remind ICO, however, that under the ITU Radio Regulations, operation of a GSO satellite in an allocated FSS band is entitled to protection against interference from co-frequency NGSO satellites only if the GSO satellite's north-south inclination is 4.5º or less. Thus, during periods in which ICO-G
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-50A1.doc http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-50A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-50A1.txt
- as much as six degrees. This inclination would decrease under the influence of gravitational forces of the sun and moon, and then would begin to increase, thereby fluctuating between about one and six degrees during the expected life of the satellite. MSV states that its satellite will operate consistent with the requirements for inclined orbit satellites set forth in Section 25.280. We will grant MSV's request. We note, however, that granting this request creates a potential for harmful interference between MSV-2's Ku-band operations and Ku-band NGSO fixed-satellite service (FSS) satellites. Pursuant to ITU Radio Regulations GSO satellites, such as MSV-2, are protected against interference from NGSO FSS satellites operating in the same band provided that GSO satellite's north-south inclination is 4.5º
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-05-50A1_Erratum.doc
- as much as six degrees. This inclination would decrease under the influence of gravitational forces of the sun and moon, and then would begin to increase, thereby fluctuating between about one and six degrees during the expected life of the satellite. MSV states that its satellite will operate consistent with the requirements for inclined orbit satellites set forth in Section 25.280. We will grant MSV's request. We note, however, that granting this request creates a potential for harmful interference between MSV-2's Ku-band operations and Ku-band NGSO fixed-satellite service (FSS) satellites. Pursuant to ITU Radio Regulations GSO satellites, such as MSV-2, are protected against interference from NGSO FSS satellites operating in the same band provided that GSO satellite's north-south inclination is 4.5º
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-07-3445A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-07-3445A1.txt
- and Ku-band frequencies (10.95-11.2 GHz and 11.45-11.7 GHz and 14.0-14.5 GHz) at the 157º E.L. orbital location, in accordance with the terms, conditions, and technical specifications set forth in its application, the attachment to grant and the Commission's rules. While at the 157º E.L. orbital location, Intelsat has indicated that the satellite will operate at inclined orbit, pursuant to Section 25.280 of the Commission's rules. S2641 SAT-STA-20070607-00078 E Effective Date: 07/23/2007 Grant of Authority Special Temporary Authority DIRECTV Enterprises, LLC Nature of Service: Other On July 23, 2007, the Policy Branch granted with conditions the request of DIRECTV Enterprises, LLC ("DIRECTV") for special temporary authority (STA), File No. SAT-STA-20070607-00078. Accordingly, DIRECTV IS AUTHORIZED, for thirty days commencing August 10, 2007, to
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-08-157A1.doc http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-08-157A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/DA-08-157A1.txt
- sharing between DoD meteorological satellite systems and non-voice, non-geostationary satellite systems in the 400.15-401 MHz band. SUBPART D-TECHNICAL OPERATIONS Brief Description: Establishes process for operating satellites in inclined orbit. Need: Informs licensees of process for operating satellites in inclined orbit mode. Legal Basis: Interprets or applies 47 U.S.C. 154, 301, 302, 303, 307, 309 and 332. Section Number and Title: 25.280 Inclined orbit operations. SUBPART F-COMPETITIVE BIDDING PROCEDURES FOR DARS Brief Description: Establishes that mutually exclusive initial applications for the satellite digital audio radio service are subject to competitive bidding. Need: Informs licensees of process for operating satellite digital audio radio service licenses. Legal Basis: Interprets or applies 47 U.S.C. 154, 301, 302, 303, 307, 309 and 332. Section Number and
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/DOC-275582A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/DOC-275582A1.txt
- the restriction in Footnote NG104), (3) Section 25.202(g) (requiring TT&C to be conducted at the edges of the operator's licensed frequency bands), and, to the extent necessary, (4) Section 25.140(b)(2) (requiring applicants for FSS operating authority to submit an interference analysis with respect to adjacent satellites at two degrees of orbital separation), (5) Section 25.210(j) (GSO station-keeping requirement), (6) Section 25.280(b)(4) (requiring GSO satellites in inclined orbits to maintain the authorized longitudinal position in the geostationary arc), and (7) completion requirements for Schedule S to FCC Form 312. Page 1 of 1
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- incorporated these operational EPFDdown limits into our Rules. Protection of operations for GSO FSS satellites inclined greater than 4.5 degrees is more difficult because inclined operations basically extend the north-south extension of the geostationary satellite orbit. However, the number of U.S. licensed satellites that continue to provide service while at inclinations greater than 4.5 degrees is extremely limited, and Section 25.280 of the Commission's Rules does not provide additional protection to GSO FSS satellites beyond that provided to GSO FSS satellites that are operating without inclination. Thus, we do not adopt specific protection requirements for GSO operations inclined beyond 4.5 degrees. However, we urge both NGSO and GSO operators to make good faith efforts to coordinate their respective operations. Protection of
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-02-80A1.doc http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-02-80A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-02-80A1.txt
- follows: 25.210 Technical requirements for space stations in the Fixed-Satellite Service. ***** (j) Space stations operated in the geostationary satellite orbit must be maintained within 0.05o of their assigned orbital longitude in the east/west direction, unless specifically authorized by the Commission to operate with a different longitudinal tolerance, and except as provided in Section 25.282 (End-of-life disposal). ***** 4. Section 25.280 is proposed to be amended in its entirety, as follows: § 25.280 Inclined Orbit Operations (a) Satellite operators may commence operation in inclined orbit mode without obtaining prior Commission authorization provided that the Commission is notified by letter within 30 days after the last north-south station keeping maneuver. The notification shall include: (1) The operator's name; (2) The date of
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-04-130A1.doc http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-04-130A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-04-130A1.txt
- further notice of proposed rulemaking to be initiated at a later date. Our action today does not, however, alter in any way the obligation of space stations in the Fixed-Satellite Service to comply with the ±0.05° longitudinal tolerance requirements of Section 25.210(j), as amended herein. The second change proposed in the Orbital Debris Notice involved amending the text of Section 25.280 of the Commission's rules. Section 25.280 permits satellite operators in geosynchronous orbits to operate in inclined orbits without prior Commission authorization, subject to certain conditions, including notification to the Commission of such operations. The Notice proposed to amend the text of this rule by specifying that notification to the Commission must occur within 30 days after the last north-south station-keeping
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-11-93A1.doc http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-11-93A1.pdf http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-11-93A1.txt
- to the same entity, although they are in no way limited to such cases. Specifically, they presume that the variation in apogee and perigee values between the two satellites do not exceed 40 km, and that the combined angular separation in the two orbits due to inclination variation is not greater that 0.15º. 47 C.F.R. § 25.210(j). 47 C.F.R. § 25.280(a). 47 C.F.R. § 25.280(b)(2). 47 C.F.R. § 25.280(b)(3). We envision that 17/24 GHz BSS satellites will frequently be used to provide services to consumers via a consumer antenna. Such consumer antennas are not capable of tracking satellites. In some instances more highly inclined orbits may be preferred during end-of-life operations. Waivers of the 0.075º inclination requirement sought by 17/24 GHz
- http://hraunfoss.fcc.gov/edocs_public/attachmatch/FCC-11-93A1_Rcd.pdf
- to the same entity, although they are in no way limited to such cases. 112Specifically, they presume that the variation in apogee and perigee values between the two satellites do not exceed 40 km, and that the combined angular separation in the two orbits due to inclination variation is not greater that 0.15º. 11347 C.F.R. § 25.210(j). 11447 C.F.R. § 25.280(a). 11547 C.F.R. § 25.280(b)(2). 11647 C.F.R. § 25.280(b)(3). 117We envision that 17/24 GHz BSS satellites will frequently be used to provide services to consumers via a consumer antenna. Such consumer antennas are not capable of tracking satellites. 8945 Federal Communications Commission FCC 11-93 the reverse-band sharing environment, however, where space path interference occurring between two networks can be significantly influenced
- http://transition.fcc.gov/Bureaus/Engineering_Technology/Orders/2000/fcc00418.doc http://transition.fcc.gov/Bureaus/Engineering_Technology/Orders/2000/fcc00418.pdf http://transition.fcc.gov/Bureaus/Engineering_Technology/Orders/2000/fcc00418.txt
- incorporated these operational EPFDdown limits into our Rules. Protection of operations for GSO FSS satellites inclined greater than 4.5 degrees is more difficult because inclined operations basically extend the north-south extension of the geostationary satellite orbit. However, the number of U.S. licensed satellites that continue to provide service while at inclinations greater than 4.5 degrees is extremely limited, and Section 25.280 of the Commission's Rules does not provide additional protection to GSO FSS satellites beyond that provided to GSO FSS satellites that are operating without inclination. Thus, we do not adopt specific protection requirements for GSO operations inclined beyond 4.5 degrees. However, we urge both NGSO and GSO operators to make good faith efforts to coordinate their respective operations. Protection of
- http://wireless.fcc.gov/auctions/53/releases/fc000418.pdf http://wireless.fcc.gov/auctions/53/releases/fc000418.txt
- incorporated these operational EPFDdown limits into our Rules.258 Protection of operations for GSO FSS satellites inclined greater than 4.5 degrees is more difficult because inclined operations basically extend the north-south extension of the geostationary satellite orbit. However, the number of U.S. licensed satellites that continue to provide service while at inclinations greater than 4.5 degrees is extremely limited,259 and Section 25.280 of the Commission's Rules does not provide additional protection to GSO FSS satellites beyond that provided to GSO FSS satellites that are operating without inclination.260 Thus, we do not adopt specific protection requirements for GSO operations (Continued from previous page) the main factors that limits a satellite's life. A satellite in inclined orbit is able to drift within a pre-defined
- http://www.fcc.gov/Bureaus/Engineering_Technology/Orders/2000/fcc00418.doc http://www.fcc.gov/Bureaus/Engineering_Technology/Orders/2000/fcc00418.pdf http://www.fcc.gov/Bureaus/Engineering_Technology/Orders/2000/fcc00418.txt
- incorporated these operational EPFDdown limits into our Rules. Protection of operations for GSO FSS satellites inclined greater than 4.5 degrees is more difficult because inclined operations basically extend the north-south extension of the geostationary satellite orbit. However, the number of U.S. licensed satellites that continue to provide service while at inclinations greater than 4.5 degrees is extremely limited, and Section 25.280 of the Commission's Rules does not provide additional protection to GSO FSS satellites beyond that provided to GSO FSS satellites that are operating without inclination. Thus, we do not adopt specific protection requirements for GSO operations inclined beyond 4.5 degrees. However, we urge both NGSO and GSO operators to make good faith efforts to coordinate their respective operations. Protection of