Showing default

ELEKTRON 1, 746

Orbit data source: Space-Track

ELEKTRON 1, 746 is a payload satellite owned by OKB-1 (CIS) that was launched on Thu, 30 Jan 1964 UTC via a VOSTOK 8K72 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Loading next visibility...
Identifier
746, 1964-006A
Orbit
Active
Country
Flag of CISCIS
Related business
Manufacturer
OKB-1
Mission
Spacecraft
Bus & Motor
OBJECT D, SRM
Mass
350 kg wet, 350 kg dry
Launch date (UTC)
1964-01-30 (63 years ago)
Launch vehicle
VOSTOK 8K72
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
DOMED CYL+ANT+PAN, 2.0 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 ELEKTRON 1
1 00746U 64006A   26251.47710547  .00000441  00000-0  12978-3 0  9993
2 00746  60.8856  75.2943 2996337 248.2719  77.5364  9.10982812 74838
Epoch: 2026-09-08T11:27Z
TLE epoch observation values (Epoch: 2026-09-08T11:27:01.912Z)
Latitude
0.00005°
Longitude
-84.0066°
Altitude
3,542.171 km
Speed
6.263 km/s
True Right ascension
05h 01m 10s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
23:32:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
6,206.738 km
Perigee altitude
403.791 km
Semi-major axis
9,683.402 km
Eccentricity
0.29963
Inclination
60.8856°
RAAN
75.2943°
Arg. of periapsis
248.2719°
True anomaly
111.81676°
Mean anomaly
77.5364°
Eccentric anomaly
94.64769°
Mean motion
2.27772 °/min
Orbital period
158.05 mins
BSTAR
0.00012978
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|