KH-11 Kennan - KH-11 Missions

KH-11 Missions

Nine KH-11 satellites were launched between 1976 and 1990 aboard Titan-3D and −34D rockets, with one launch failure. For the following five satellite launches between 1992 and 2005, a Titan IV launch vehicle was used. The most recent launch in 2011 was carried out by a Delta IV Heavy rocket. The KH-11 replaced the KH-9 film return satellite, among others, the last of which was lost in a liftoff explosion in 1986.

KH-11 satellites are in either of two standard planes in Sun-synchronous orbits. As shadows help to discern ground features, satellites in a standard plane east of a noon/midnight orbit observe the ground at local afternoon hours, while satellites in a western plane observe the ground at local morning hours. Historically launches have therefore been timed to occur either about two hours before or one hour after local noon (or midnight), respectively.

Name KH-11
Block
Launch date ID NROL number Orbit Plane Orbital decay date
OPS 5705 1-1 19 December 1976 1976-125A N/A 247 km × 533 km, i=96.9° West 28 January 1979
OPS 4515 1–2 14 June 1978 1978-060A 276 km × 509 km, i=96.8° West 23 August 1981
OPS 2581 1–3 7 February 1980 1980-010A 309 km × 501 km, i=97.1° East 30 October 1982
OPS 3984 1–4 3 September 1981 1981-085A 244 km × 526 km, i=96.9° West 23 November 1984
OPS 9627 1–5 17 November 1982 1982-111A 280 km × 522 km, i=96.9° East 13 August 1985
USA-6 2-1 4 December 1984 1984-122A 335 km × 758 km, i=98° West 10 November 1994
Unknown 2-2 28 August 1985 N/A Failed to orbit East N/A
USA-27 2–3 26 October 1987 1987-090A 300 km × 1000 km, i=98° East 11 June 1992
USA-33 2–4 6 November 1988 1988-099A 300 km × 1000 km, i=98° West 12 May 1996
USA-86 3-1 28 November 1992 1992-083A 408 km × 931 km, i=97.7° East 5 June 2000
USA-116 3-2 5 December 1995 1995-066A 405 km × 834 km, i=97.7° East 19 November 2008
USA-129 3-3 20 December 1996 1996-072A NROL-2 292 km × 894 km, i=97.7° West
USA-161 4-1 5 October 2001 2001-044A NROL-14 309 km × 965 km, i=97.9° East
USA-186 3–4 19 October 2005 2005-042A NROL-20 256 km × 1006 km, i=97.9° West
USA-224 4-2 20 January 2011 2011-002A NROL-49 290 km × 985 km, i=97.9° East

KH-11 satellites require periodic reboosts to counter atmospheric drag, or to adjust their ground track to surveillance requirements. Based on data collected by amateur observers, the following orbital characteristics of OPS 5705 were calculated by amateur skywatcher Ted Molczan.

OPS 5705
Time period
Periapsis
(AMSL)
Apoapsis
(AMSL)
Apogee at end of period
(AMSL)
19 December 1976 – 23 December 253 km (157 mi) 541 km (336 mi) 541 km (336 mi)
23 December 1976 – 27 March 1977 348 km (216 mi) 541 km (336 mi) 537 km (334 mi)
27 March 1977 – 19 August 270 km (170 mi) 537 km (334 mi) 476 km (296 mi)
19 August 1977–1978 January 270 km (170 mi) 528 km (328 mi) 454 km (282 mi)
1978 January – 28 January 1979 263 km (163 mi) 534 km (332 mi) Deorbited

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