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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.

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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 (62 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: 4 hours ago

TLE from 4 hours ago
0 ELEKTRON 3
1   829U 64038A   26092.88232308  .00001447  00000-0  40665-3 0  9993
2   829  60.8168 305.2023 2938650 328.8475  16.6713  9.21154649  8514
Epoch: 2026-04-02T21:10Z
TLE epoch observation values (Epoch: 2026-04-02T21:10:32.714Z)
Latitude
Longitude
156.34156°
Altitude
642.561 km
Speed
8.492 km/s
True Right ascension
20h 20m 48s
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
06:27:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
6,058.474 km
Perigee altitude
409.222 km
Semi-major axis
9,611.985 km
Eccentricity
0.29387
Inclination
60.8168°
RAAN
305.2023°
Arg. of periapsis
328.8475°
True anomaly
31.24391°
Mean anomaly
16.6713°
Eccentric anomaly
23.34272°
Mean motion
2.30316 °/min
Orbital period
156.31 mins
BSTAR
0.00040665
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