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Intelsat 5
Intelsat 5 F-1
Intelsat 5 F-1
Credit: Manufacturer Image
American communications satellite. The last five of the nine spacecraft in this block carry a maritime mobile payload (seven additional transponders) for lease by Inmarsat. Built by Ford Aerospace for Intelsat, International. Launched 1980 - 1984. Used Intelsat-5 bus.

Status: Operational 1980. First Launch: 1980-12-06. Last Launch: 1984-06-09. Number: 9 . Gross mass: 2,000 kg (4,400 lb). Height: 2.00 m (6.50 ft). Span: 15.90 m (52.10 ft).

Spacecraft: 3-axis stabilized to 0.5 deg using momentum wheels. Hydrazine propulsion system. Passive thermal control. Dual solar arrays provide 1800 W BOL, NiCd or NiH batteries. Payload: 21 C-Band and 4 Ku-Band transponders.12000 voice circuits and 2 TV channels.
Financial/Operational:
5f series


More at: Intelsat 5.

Subtopics

Intelsat 5A American communications satellite. The Intelsat 5A series was derived from the Intelsat 5. Communication satellite built by Ford Aerospace for Intelsat / New Skies (NSS) / Columbia, International. Launched 1985 - 1989. Used Intelsat-5 bus.

Family: Communications, Geosynchronous orbit. Country: USA. Engines: Star 37F. Launch Vehicles: Atlas, Atlas SLV-3D Centaur, Ariane 1, Ariane, Atlas G Centaur. Projects: Intelsat. Launch Sites: Cape Canaveral, Cape Canaveral LC36A, Cape Canaveral LC36B, Kourou, Kourou ELA1. Agency: Inmarsat, Aeronutronics. Bibliography: 2, 278, 279, 6, 6594, 12667.
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Panamsat 5Panamsat 5
Credit: Manufacturer Image



1980 December 6 - . 23:31 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas SLV-3D Centaur.
  • Intelsat 5 F-2 - . Mass: 2,000 kg (4,400 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. Completed Operations Date: 1998-04-17 . USAF Sat Cat: 12089 . COSPAR: 1980-098A. Apogee: 36,242 km (22,519 mi). Perigee: 36,118 km (22,442 mi). Inclination: 9.7000 deg. Period: 1,456.20 min.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit at 21 deg W in 1981; 27 deg W in 1981-1983; 34 deg W in 1983-1985; 27 deg W in 1985; 1 deg W in 1985-1989; 21 deg W in 1989-1994; 40 deg W in 1994-1998 As of 2 September 2001 located at 103.82 deg W drifting at 5.004 deg W per day. As of 2007 Mar 10 located at 81.84W drifting at 5.000W degrees per day.


1981 May 23 - . 22:42 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas SLV-3D Centaur.
  • Intelsat 5 F-1 - . Payload: Intelsat 501. Mass: 1,928 kg (4,250 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. Completed Operations Date: 1997-02-08 . USAF Sat Cat: 12474 . COSPAR: 1981-050A. Apogee: 36,224 km (22,508 mi). Perigee: 36,151 km (22,463 mi). Inclination: 10.1000 deg. Period: 1,456.60 min.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit at 24 deg W in 1981; 60 deg E in 1982-1984; 57 deg E in 1984-1986; 174 deg E in 1986-1988; 177 deg E in 1988-1990; 177 deg W in 1990-1992; 91 deg E in 1993-1996; 72 deg E in 1996-1997 As of 4 September 2001 located at 169.69 deg W drifting at 5.095 deg W per day. As of 2007 Mar 10 located at 13.28E drifting at 5.096W degrees per day.


1981 December 15 - . 23:35 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas SLV-3D Centaur.
  • Intelsat 5 F-3 - . Mass: 1,870 kg (4,120 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. Completed Operations Date: 1998-01-19 . USAF Sat Cat: 12994 . COSPAR: 1981-119A. Apogee: 36,129 km (22,449 mi). Perigee: 35,894 km (22,303 mi). Inclination: 9.4000 deg. Period: 1,447.60 min.

    Positioned in geosynchronous orbit at 24 deg W in 1982-1985; 27 deg W in 1985; 53 deg W in 1985-1988; 174 deg E in 1988-1990; 177 deg E in 1990-1992; 177 deg W in 1992-1995; 157 deg E in 1995-1998 As of 5 September 2001 located at 57.52 deg W drifting at 2.890 deg W per day. As of 2007 Mar 9 located at 101.94W drifting at 2.904W degrees per day.


1982 March 5 - . 00:23 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas SLV-3D Centaur.
  • Intelsat 5 F-4 - . Mass: 1,928 kg (4,250 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. Completed Operations Date: 1995-11-28 . USAF Sat Cat: 13083 . COSPAR: 1982-017A. Apogee: 36,243 km (22,520 mi). Perigee: 35,920 km (22,310 mi). Inclination: 9.4000 deg. Period: 1,451.20 min.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit at 32 deg E in 1982; 63 deg E in 1982; 27 deg W in 1983-1985; 34 deg W in 1985-1992; 40 deg W in 1992; 31 deg W in 1993-1995; 29 deg W in 1995 As of 1 September 2001 located at 4.64 deg W drifting at 3.747 deg W per day. As of 2007 Mar 7 located at 4.34W drifting at 3.748W degrees per day.


1982 September 28 - . 23:17 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas SLV-3D Centaur.
  • Intelsat 5 F-5 - . Mass: 2,000 kg (4,400 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. USAF Sat Cat: 13595 . COSPAR: 1982-097A. Apogee: 36,404 km (22,620 mi). Perigee: 36,228 km (22,510 mi). Inclination: 9.0000 deg. Period: 1,463.30 min.

    Positioned in geosynchronous orbit at 63 deg E in 1982-1990; 66 deg E in 1991-1996; 33 deg E in 1996; 72 deg E in 1997-on. As of 3 September 2001 located at 16.28 deg E drifting at 6.707 deg W per day. As of 2007 Mar 9 located at 163.88W drifting at 6.709W degrees per day.


1983 May 19 - . 22:26 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas SLV-3D Centaur.
  • Intelsat 5 F-6 - . Mass: 1,928 kg (4,250 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. Completed Operations Date: 1998-07-06 . USAF Sat Cat: 14077 . COSPAR: 1983-047A. Apogee: 36,125 km (22,446 mi). Perigee: 36,076 km (22,416 mi). Inclination: 8.3000 deg. Period: 1,452.10 min.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit at 29 deg E in 1983; 18 deg W in 1983-1992; 34 deg W in 1992; 50 deg W in 1992-1995; 31 deg W in 1995-1998 As of 4 September 2001 located at 47.96 deg E drifting at 3.999 deg W per day. As of 2007 Mar 10 located at 62.15W drifting at 3.995W degrees per day.


1983 October 19 - . 00:45 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 1.
  • Intelsat 5 F-7 - . Mass: 1,928 kg (4,250 lb). Nation: International. Agency: INTELSAT. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. Completed Operations Date: 1996-07-23 . USAF Sat Cat: 14421 . COSPAR: 1983-105A. Apogee: 35,972 km (22,351 mi). Perigee: 35,928 km (22,324 mi). Inclination: 8.5000 deg. Period: 1,444.50 min.

    Ariane third stage. Launched by European Space Agency. Launch time 0045:36 GMT. Launched spacecraft Intelsat V F7. Positioned in geosynchronous orbit at 60 deg E in 1984-1985; 66 deg E in 1985-1991; 57 deg E in 1991-1995; 47 deg E in 1995-1996 As of 28 August 2001 located at 140.34 deg E drifting at 2.062 deg W per day. As of 2007 Mar 9 located at 88.83W drifting at 2.097W degrees per day.


1984 March 5 - . 00:50 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 1.
  • Intelsat 5 F-8 - . Mass: 1,928 kg (4,250 lb). Nation: International. Agency: INTELSAT. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. Completed Operations Date: 1994-12-17 . USAF Sat Cat: 14786 . COSPAR: 1984-023A. Apogee: 36,755 km (22,838 mi). Perigee: 36,531 km (22,699 mi). Inclination: 8.2000 deg. Period: 1,480.10 min. Positioned in geosynchronous orbit at 53 deg W in 1984-1985; 180 deg E in 1985-1994 As of 28 August 2001 located at 164.20 deg W drifting at 10.735 deg W per day. As of 2007 Mar 11 located at 110.10E drifting at 10.740W degrees per day..

1984 June 9 - . 23:03 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas G Centaur. FAILURE: Centaur structural failure. . Failed Stage: U.
  • Intelsat 5 F-9 - . Mass: 1,091 kg (2,405 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 5. Decay Date: 1984-10-24 . USAF Sat Cat: 15034 . COSPAR: 1984-057A. Apogee: 1,227 km (762 mi). Perigee: 180 km (110 mi). Inclination: 29.2000 deg. Period: 98.90 min. Failure of Centaur upper stage left stranded in useless orbit. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle was to have put payload into geosynchronous transfer orbit.

1985 March 22 - . 23:58 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas G Centaur.
  • Intelsat 5A F-10 - . Mass: 2,013 kg (4,437 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Intelsat 5. Spacecraft: Intelsat 5A. USAF Sat Cat: 15629 . COSPAR: 1985-025A. Apogee: 36,468 km (22,660 mi). Perigee: 36,237 km (22,516 mi). Inclination: 7.2000 deg. Period: 1,465.10 min.

    Positioned in geosynchronous orbit at 24 deg W in 1985-1990; 174 deg E in 1990-1994; 66 deg E in 1994-1995; 57 deg E in 1995-1996; 33 deg E in 1996-1999 As of 5 September 2001 located at 135.23 deg W drifting at 7.152 deg W per day. As of 2007 Mar 9 located at 107.21W drifting at 7.157W degrees per day.


1985 June 30 - . 00:44 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas G Centaur.
  • Intelsat 5A F-11 - . Mass: 1,098 kg (2,420 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Intelsat 5. Spacecraft: Intelsat 5A. USAF Sat Cat: 15873 . COSPAR: 1985-055A. Apogee: 35,799 km (22,244 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.7000 deg. Period: 1,436.10 min.

    Positioned in geosynchronous orbit at 27 deg W in 1985-1990; 63 deg E in 1990-1992; 177 deg E in 1992-1994; 180 deg E in 1994-1997; 29 deg W in 1998-1999 As of 4 September 2001 located at 29.54 deg W drifting at 0.005 deg W per day. As of 2007 Mar 9 located at 113.07W drifting at 0.696W degrees per day.


1985 September 28 - . 23:36 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. LV Family: Atlas. Launch Vehicle: Atlas G Centaur.
  • Intelsat 5A F-12 - . Mass: 1,096 kg (2,416 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Intelsat 5. Spacecraft: Intelsat 5A. Completed Operations Date: 1998-06-23 . USAF Sat Cat: 16101 . COSPAR: 1985-087A. Apogee: 36,140 km (22,450 mi). Perigee: 36,086 km (22,422 mi). Inclination: 6.2000 deg. Period: 1,452.80 min.

    Telephone communications; 31 deg E. Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit at 60 deg E in 1985-1989; 1 deg W in 1989-1994; 21 deg W in 1994-1996; 56 deg W in 1996-1998 As of 28 August 2001 located at 145.57 deg E drifting at 4.159 deg W per day. As of 2007 Mar 10 located at 19.14E drifting at 4.163W degrees per day.


1986 May 31 - . 00:53 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 2. FAILURE: Third stage ignition failure. Destroyed by range safety.. Failed Stage: U.
1988 May 17 - . 23:58 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 2.
  • Intelsat 5A F-13 - . Mass: 2,013 kg (4,437 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Intelsat 5. Spacecraft: Intelsat 5A. USAF Sat Cat: 19121 . COSPAR: 1988-040A. Apogee: 35,800 km (22,200 mi). Perigee: 35,776 km (22,230 mi). Inclination: 0.1000 deg. Period: 1,436.20 min.

    Replaced Intelsat 5 F-3; 53 deg W. Positioned in geosynchronous orbit at 53 deg W in 1988-1995; 177 deg W in 1995-1999 As of 5 September 2001 located at 177.08 deg W drifting at 0.009 deg W per day. As of 2007 Mar 8 located at 44.56W drifting at 6.109W degrees per day.


1989 January 27 - . 01:21 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 2.
  • Intelsat 5A F-15 - . Mass: 1,977 kg (4,358 lb). Nation: International. Agency: Intelsat. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: Intelsat 5. Spacecraft: Intelsat 5A. USAF Sat Cat: 19772 . COSPAR: 1989-006A. Apogee: 35,801 km (22,245 mi). Perigee: 35,773 km (22,228 mi). Inclination: 0.0000 deg. Period: 1,436.20 min.

    International communications; 18 deg W. Positioned in geosynchronous orbit at 60 deg E in 1989-1992; 18 deg W in 1992-1996; 22 deg W in 1996-1997; 38 deg W in 1998-1999 As of 5 September 2001 located at 37.72 deg W drifting at 0.020 deg W per day. As of 2007 Mar 9 located at 153.76E drifting at 4.192W degrees per day.



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