|Mission type||Earth science|
|Launch mass||138 kg (304 lb)|
|Start of mission|
|Launch date||4 October 1964, 03:45UTC|
|Launch site||Cape Canaveral LC-17A|
|End of mission|
|Last contact||October 13, 1965|
|Decay date||January 1, 1966|
|Perigee altitude||917 km (570 mi)|
|Apogee altitude||94,288 km (58,588 mi)|
|Epoch||3 October 1964|
Explorer 21, also called IMP-B and Interplanetary Monitoring Platform IMP-B, was an American satellite launched as part of Explorers program. Explorer 21 was launched on 4 October 1964 from Cape Canaveral, Florida, United States, with a Delta rocket. Explorer 21 was the second satellite of the Interplanetary Monitoring Platform, and used the same general design as its predecessor, Explorer 18 (IMP-A), launched the previous year. The following Explorer 28 (IMP-C), launched in 1965, also used a similar design.
Explorer 21 was a solar cell and chemical-battery powered spacecraft instrumented for interplanetary and distant magnetospheric studies of energetic particles, cosmic rays, magnetic fields, and plasmas. Each normal telemetry sequence of 81.9 s in duration consisted of 795 data bits. After every third normal sequence there was an 81.9-s interval of rubidium vapor magnetometer analog data transmission. Initial spacecraft parameters included a local time of apogee at noon, a spin rate of 14.6 rpm, and a spin direction of 41.4-deg right ascension and 47.4-deg declination. The significant deviation of the spin rate and direction from the planned values and the achievement of an apogee of less than half the planned value adversely affected data usefulness.
Otherwise, spacecraft systems performed well, with nearly complete data transmission for the first 4 months and for the sixth month after launch. Data transmission was intermittent for other times, and the final transmission occurred on October 13, 1965.