ELEKTRON 3, 829
Orbit data source: Space-Track
ELEKTRON 3, 829 is a payload satellite owned by OKB-1 (CIS) in HEO that was launched on Fri, 10 Jul 1964 UTC via a VOSTOK 8K72 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payloads include a variety of satellites, spacecraft, and rockets 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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ELEKTRON 3 details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 14 hours ago |
| Origin | |
| Manufacturer | OKB-1 |
| Mission status | Unknown |
| Mission | Civil Science |
| Bus & Motor | OBJECT D, Unknown motor |
| Mass | 350 kg wet, 350 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Radar Cross Section | 2.8 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 14 hours ago
0 ELEKTRON 3
1 00829U 64038A 24251.50358129 .00006997 00000-0 19525-2 0 9992
2 00829 60.8182 16.4345 2949657 175.5824 187.8783 9.18617794955837Epoch: 2024-09-07T12:05Z
Definitive object data (Epoch: 2024-09-07T12:05:09.423Z)
| Latitude | 0.00003° |
| Longitude | -151.91557° |
| Altitude | 6,078.423 km |
| Speed | 4.756 km/s |
| True Right ascension | 01h 05m 44s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Predictive object data (real-time)
| Latitude | 57.69829° |
| Longitude | -91.10777° |
| Altitude | 2,921.693 km |
| Speed | 6.667 km/s |
| Apparent Right ascension | 05h 36m 46s |
| Apparent Declination | 21° 01' 07" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 18:05:02 |
| Azimuth | 7.521° NNE |
| Elevation | -28.71° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 6,091.962 km |
| Perigee | 411.114 km |
| Semi-major axis | 9,629.675 km |
| Eccentricity | 0.2949657 |
| Inclination | 60.8182° |
| RAAN | 16.4345° |
| Arg. of periapsis | 175.5824° |
| True anomaly | 184.49285° |
| Mean anomaly | 187.8783° |
| Eccentric anomaly | 186.0864° |
| Mean motion | 2.29681 °/min |
| BSTAR | 0.0019525 |
| Period | 156.74 mins |
No data available
Other satellites on launch #38 in the year 1964 (1964-07-10 UTC)
| ELEKTRON 3, 829 |
| ELEKTRON 4, 830 (Decayed) |
| ELEKTRON 3 DEB, 831 |
| SL-3 R/B, 832 (Decayed) |
| ELEKTRON 3 DEB, 5892 (Decayed) |
| ELEKTRON 3 DEB, 5893 (Decayed) |
| ELEKTRON 3 DEB, 29008 |
ELEKTRON 3 Visibility forecast
Observer location: 39.9160978°, -105.1181434
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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