Showing default

ELEKTRON 3, 829

Orbit data source: Space-Track

ELEKTRON 3, 829 is a payload satellite owned by OKB-1 (CIS) that was launched on Fri, 10 Jul 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
829, 1964-038A
Orbit
Active
Country
Flag of CISCIS
Related business
Manufacturer
OKB-1
Mission
Spacecraft
Bus & Motor
OBJECT D, Unknown motor
Mass
350 kg wet, 350 kg dry
Launch date (UTC)
1964-07-10 (61 years ago)
Launch vehicle
VOSTOK 8K72
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 ELEKTRON 3
1 00829U 64038A   25334.64077227  .00001111  00000-0  31879-3 0  9997
2 00829  60.8159 115.7958 2940197 295.8478  36.9007  9.20663659997153
Epoch: 2025-11-30T15:22Z
TLE epoch observation values (Epoch: 2025-11-30T15:22:42.724Z)
Latitude
-0.00005°
Longitude
175.36604°
Altitude
1,413.171 km
Speed
7.804 km/s
True Right ascension
07h 43m 10s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
18:49:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
6,064.384 km
Perigee altitude
410.148 km
Semi-major axis
9,615.403 km
Eccentricity
0.29402
Inclination
60.8159°
RAAN
115.7958°
Arg. of periapsis
295.8478°
True anomaly
64.24684°
Mean anomaly
36.9007°
Eccentric anomaly
49.7601°
Mean motion
2.30193 °/min
Orbital period
156.39 mins
BSTAR
0.00031879
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|