Mission type | Solar physics |
---|---|
Operator | DoD Space Test Program[1] |
COSPAR ID | 1979-017A[2] |
SATCAT no. | 11278[2] |
Mission duration | 6 years, 6 months, 20 days |
Spacecraft properties | |
Manufacturer | Ball Aerospace |
Launch mass | 1,331 kilograms (2,934 lb)[3] |
Dry mass | 850 kilograms (1,870 lb) |
Start of mission | |
Launch date | February 24, 1979, 08:24:00[3] | UTC
Rocket | Atlas F |
Launch site | Vandenberg, SLC-3W[3] |
End of mission | |
Disposal | Destroyed by ASAT |
Destroyed | September 13, 1985 |
Orbital parameters | |
Reference system | Sun-synchronous[4] |
Regime | Low Earth |
Eccentricity | .0022038[5] |
Perigee altitude | 515 kilometres (320 mi)[5] |
Apogee altitude | 545 kilometres (339 mi)[5] |
Inclination | 97.6346°[5] |
RAAN | 182.5017[5] |
Argument of perigee | 99.6346[5] |
Mean anomaly | 260.9644[5] |
Mean motion | 15.11755304[5] |
Epoch | 1985 09 13.72413718[5] |
Instruments | |
Gamma-ray spectrometer, a white light spectrograph, an extreme ultraviolet spectrometer, a high latitude particle spectrometer, an aerosol monitor, and an X-ray monitor[4] | |
P78-1 or Solwind was a United States satellite launched aboard an Atlas F rocket from Vandenberg Air Force Base in California on February 24, 1979.[6] The satellite's mission was extended by several weeks, so that it operated until it was destroyed in orbit on September 13, 1985, to test the ASM-135 ASAT anti-satellite missile.
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was invoked but never defined (see the help page).