Iridium
Program: Iridium. Objective: Communications. The Iridium system is a planned commercial communications network comprised of a constellation of 66 LEO spacecraft. The system will use L-Band to provide global communications services through portable handsets. A total of 125 spacecraft will be built by Lockheed for more than $700M. Commercial service are planned to begin in 1998. Total cost of the project is estimated at $3.45 billion and subscriber fees are estimated at $3 per minute. The system will employ 15-20 ground stations with a master control complex in Landsdowne, VA, a backup in Italy, and a third engineering centre in Chandler, AZ.
Financial/Operational:
6 planes x 11 satellites + 6 spares. Delta II Vandenberg launch of 5 Iridium mobile satellites #4 to #8
Financial/Operational:
Delta 2 launch 5 Motorola satellites from Vandenberg. Ir launch #7, 39 units in orbit.
Financial/Operational:
Delta 2 launch ninth/final 1997 5 units Iridium (46 units for 1997)
Financial/Operational:
China Long March 2 C band two stage booster launch 2 satellites, 41 unit launch - 3 suspect.
Financial/Operational:
Proton launch 7 units from Baikonur (2nd set Iridiums)
Financial/Operational:
Delta II Vandenberg launch of 5 Iridium mobile satellites- third set
Financial/Operational:
Delta II Vandenberg launch of 5 Iridium mobile satellites- fourth set (22 to 26).
Major Events:

  • 1997 May 5 - Iridium 4.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.5 degrees.

  • 1997 May 5 - Iridium 5.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.5 degrees.

  • 1997 May 5 - Iridium 6.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.5 degrees.

  • 1997 May 5 - Iridium 7.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.4 degrees.

  • 1997 May 5 - Iridium 8.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.5 degrees.

  • 1997 June 18 - Iridium 13.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 5. Ascending node 294.2 degrees.

  • 1997 June 18 - Iridium 10.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 5. Ascending node 294 degrees.

  • 1997 June 18 - Iridium 11.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 5. Ascending node 294.6 degrees. Not in service.

  • 1997 June 18 - Iridium 16.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 5. Ascending node 294.2 degrees.

  • 1997 June 18 - Iridium 9.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 5. Ascending node 294.2 degrees.

  • 1997 June 18 - Iridium 14.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 5. Ascending node 294.2 degrees. Not in service.

  • 1997 June 18 - Iridium 12.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 5. Ascending node 294.2 degrees.

  • 1997 July 9 - Iridium 15.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.8 degrees.

  • 1997 July 9 - Iridium 17.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.8 degrees.

  • 1997 July 9 - Iridium 21.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 310.4 degrees. Failed in low orbit.

  • 1997 July 9 - Iridium 20.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.7 degrees. Failed.

  • 1997 July 9 - Iridium 18.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.8 degrees.

  • 1997 August 21 - Iridium 25.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.4 degrees.

  • 1997 August 21 - Iridium 26.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.4 degrees.

  • 1997 August 21 - Iridium 23.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.4 degrees.

  • 1997 August 21 - Iridium 22.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.3 degrees.

  • 1997 August 21 - Iridium 24.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.3 degrees. Should be 24905, failed.

  • 1997 September 1 - Iridium.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 5. Ascending node 272 degrees. Dummy satellite.

  • 1997 September 1 - Iridium.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 5. Ascending node 271.9 degrees. Dummy satellite.

  • 1997 September 14 - Iridium 29.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 3. Ascending node 230.9 degrees.

  • 1997 September 14 - Iridium 32.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 3. Ascending node 230.9 degrees.

  • 1997 September 14 - Iridium 30.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 3. Ascending node 230.8 degrees.

  • 1997 September 14 - Iridium 31.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 3. Ascending node 230.9 degrees.

  • 1997 September 14 - Iridium 33.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 3. Ascending node 230.9 degrees.

  • 1997 September 14 - Iridium 28.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 3. Ascending node 230.9 degrees.

  • 1997 September 14 - Iridium 27.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 3. Ascending node 223.2 degrees. Failed in low orbit.

  • 1997 September 27 - Iridium 35.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.5 degrees.

  • 1997 September 27 - Iridium 34.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.5 degrees.

  • 1997 September 27 - Iridium 37.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.6 degrees.

  • 1997 September 27 - Iridium 36.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.4 degrees.

  • 1997 September 27 - Iridium 19.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 4. Ascending node 262.4 degrees.

  • 1997 November 9 - Iridium 41.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.8 degrees.

  • 1997 November 9 - Iridium 40.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.8 degrees.

  • 1997 November 9 - Iridium 39.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.8 degrees.

  • 1997 November 9 - Iridium 38.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.6 degrees.

  • 1997 November 9 - Iridium 43.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.8 degrees.

  • 1997 December 8 - Iridium 44.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 6. Ascending node 325.8 degrees. Not in service.

  • 1997 December 8 - Iridium 42.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 6. Ascending node 325.8 degrees.

  • 1997 December 20 - Iridium 46.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.4 degrees. Should be 25105.

  • 1997 December 20 - Iridium 47.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.4 degrees.

  • 1997 December 20 - Iridium 49.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.4 degrees.

  • 1997 December 20 - Iridium 48.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.4 degrees.

  • 1997 December 20 - Iridium 45.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 2. Ascending node 199.4 degrees.

  • 1998 February 18 - Iridium 56.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 294 degrees.

  • 1998 February 18 - Iridium 52.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 294.1 degrees.

  • 1998 February 18 - Iridium 53.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 294.2 degrees.

  • 1998 February 18 - Iridium 54.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 294.2 degrees.

  • 1998 February 18 - Iridium 50.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 294.2 degrees.

  • 1998 March 25 - Iridium 51.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 4. Ascending node 262.5 degrees. Not in service.

  • 1998 March 25 - Iridium 61.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 4. Ascending node 262.5 degrees.

  • 1998 March 30 - Iridium 55.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 3. Ascending node 230.9 degrees.

  • 1998 March 30 - Iridium 57.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 3. Ascending node 230.9 degrees.

  • 1998 March 30 - Iridium 58.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 3. Ascending node 230.9 degrees.

  • 1998 March 30 - Iridium 59.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 3. Ascending node 230.9 degrees.

  • 1998 March 30 - Iridium 60.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 3. Ascending node 230.9 degrees.

  • 1998 April 7 - Iridium 67.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 1. Ascending node 167.8 degrees.

  • 1998 April 7 - Iridium 66.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 1. Ascending node 167.8 degrees.

  • 1998 April 7 - Iridium 68.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    The Proton launch vehicle placed the Iridium cluster and the Block DM2 stage into low parking orbit. The DM2 fired twice to enter the deployment orbit and dispensed the seven satellites, which used their own propulsion units to reach operational altitude. The DM2 stage then fired again to deorbit itself, to avoid creating space debris. SV068 placed in Plane 1. Ascending node 167.8 degrees.

  • 1998 April 7 - Iridium 64.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 1. Ascending node 167.6 degrees.

  • 1998 April 7 - Iridium 63.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 1. Ascending node 167.8 degrees.

  • 1998 April 7 - Iridium 62.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 1. Ascending node 167.9 degrees.

  • 1998 April 7 - Iridium 65.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Baikonur. Launch Vehicle: Proton 8K82K / 17S40.

    Plane 1. Ascending node 167.9 degrees.

  • 1998 May 2 - Iridium 69.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 2. Ascending node 199.4 degrees. Not in service.

  • 1998 May 2 - Iridium 71.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 2. Ascending node 199.3 degrees. Not in service.

  • 1998 May 17 - Iridium 70.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 1. Ascending node 167.8 degrees.

  • 1998 May 17 - Iridium 72.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 1. Ascending node 167.8 degrees.

  • 1998 May 17 - Iridium 73.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 1. Ascending node 167.8 degrees.

  • 1998 May 17 - Iridium 74.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 1. Ascending node 167.8 degrees.

  • 1998 May 17 - Iridium 75.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 1. Ascending node 167.7 degrees. Not in service.

  • 1998 August 19 - Iridium 3.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 2. Ascending node 199.4 degrees.

  • 1998 August 19 - Iridium 76.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 2. Ascending node 199.4 degrees.

  • 1998 September 8 - Iridium 81.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.7 degrees.

  • 1998 September 8 - Iridium 82.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.6 degrees. Not in service.

  • 1998 September 8 - Iridium 79.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 316.3 degrees. Failed in low orbit.

  • 1998 September 8 - Iridium 77.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.4 degrees. Not in service.

  • 1998 September 8 - Iridium 80.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 6. Ascending node 325.7 degrees.

  • 1998 November 6 - Iridium 2.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 289.1 degrees. Parking orbit.

  • 1998 November 6 - Iridium 83.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 294.2 degrees.

  • 1998 November 6 - Iridium 84.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 294.1 degrees. Raising orbit.

  • 1998 November 6 - Iridium 85.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 291.1 degrees. Parking orbit.

  • 1998 November 6 - Iridium 86.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Plane 5. Ascending node 293.9 degrees. Raising orbit.

  • 1998 December 19 - Iridium 11.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 2. Ascending node 197 degrees. Parking orbit.

  • 1998 December 19 - Iridium 20.  Spacecraft: LM 700. Mass: 689 kg (1,518 lb). Launch Site: Taiyuan. Launch Vehicle: CZ-2C/SD.

    Plane 2. Ascending node 197.2 degrees. Parking orbit.

  • 2002 February 11 - Iridium .  Spacecraft: LM 700. Mass: 690 kg (1,520 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

  • 2002 February 11 - Iridium .  Spacecraft: LM 700. Mass: 690 kg (1,520 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

  • 2002 February 11 - Iridium .  Spacecraft: LM 700. Mass: 690 kg (1,520 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

  • 2002 February 11 - Iridium .  Spacecraft: LM 700. Mass: 690 kg (1,520 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

  • 2002 February 11 - Iridium .  Spacecraft: LM 700. Mass: 690 kg (1,520 lb). Launch Site: Vandenberg. Launch Vehicle: Delta 7000.

    Mobile Telephony satellite. Return to flight after GEM solid booster failure on GBI launch. Launch delayed from February 8, 9 and 10. Five Motorola Iridium satellites were launched for Iridium Satellite LLC, the new company that bought out the bankrupt Iridium LLC. This was the first system replenishment launch since the bankruptcy.

  • 2002 June 20 - Iridium SV98 .  Spacecraft: LM 700. Mass: 690 kg (1,520 lb). Launch Site: Plesetsk. Launch Vehicle: Rokot.

  • 2002 June 20 - Iridium SV97 .  Spacecraft: LM 700. Mass: 690 kg (1,520 lb). Launch Site: Plesetsk. Launch Vehicle: Rokot.

    Launch delayed from June 6, 19. The two Iridium replacement mobile telephone satellites were owned by Iridium Satellite LLC, the successor to bankrupt Iridium LLC.

 
 
 
 
 
 
 
 
 

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