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ELEKTRON 1

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ELEKTRON 1 is classified as:


NORAD ID: 746
Int'l Code: 1964-006A
Perigee: 414.3 km
Apogee: 6,317.4 km
Inclination: 60.9 °
Period: 159.4 minutes
Semi major axis: 9736 km
RCS: 2.7554 m2 (large)
Launch date: January 30, 1964
Source: Commonwealth of Independent States (former USSR) (CIS)
Launch site: TYURATAM MISSILE AND SPACE COMPLEX (TTMTR)

Electron 1 was launched with Electron 2 by a single launch vehicle in order to perform simultaneous investigations of the external and internal zones of the Earth's radiation belt. Electron 1 had a cylindrical body that was 0.75 m in diameter and 1.3 m long and from which antennas and six solar cell panels were extended. The spacecraft was placed into an eccentric orbit that enabled it to study the internal zone of the radiation belt. It was equipped with micrometeorite detectors, a mass spectrometer, a proton detector, and instruments for recording the corpuscular emission and energy spectrum of electrons. A memory device was included so that observations over several orbits could be obtained by USSR telemetry stations when the satellite was within communications range.
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NASA's NSSDC Master Catalog

Two Line Element Set (TLE):
1   746U 64006A   19140.17412108  .00000125  00000-0  49156-4 0  9999
2   746  60.8616  64.1613 3031291 286.3451  42.8473  9.03597810833032
Source of the keplerian elements: AFSPC