ELEKTRON 1

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ELEKTRON 1 is classified as:

Space & Earth Science

NORAD ID: 746

Int'l Code: 1964-006A

Perigee: 407.1 km

Apogee: 6,249.7 km

Inclination: 60.9 °

Period: 158.4 minutes

Semi major axis: 9699 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.

1 00746U 64006A   25021.78117974  .00002823  00000-0  72003-3 0  9997
2 00746  60.8601 160.9158 3011854  96.1914 298.5209  9.08840636 20700

Source of the keplerian elements: AFSPC