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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829 intel report (Beta)
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ELEKTRON 3 details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 20 hours ago |
| Origin | |
| Manufacturer | OKB-1 |
| 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 |
| Shape & HBR | Cyl + 6 Pan, 4 m |
| Radar Cross Section | 2.718 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 20 hours ago
0 ELEKTRON 3
1 00829U 64038A 24291.43969834 .00003929 00000-0 11147-2 0 9993
2 00829 60.8135 321.3968 2946507 186.2269 169.2275 9.19023189959505Epoch: 2024-10-17T10:33Z
Definitive object data (Epoch: 2024-10-17T10:33:09.936Z)
| Latitude | 0.00002° |
| Longitude | 136.68166° |
| Altitude | 6,057.666 km |
| Speed | 4.766 km/s |
| True Right ascension | 21h 25m 35s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | 23.20542° |
| Longitude | -58.21597° |
| Altitude | 676.123 km |
| Speed | 8.466 km/s |
| Apparent Right ascension | 10h 18m 47s |
| Apparent Declination | -7° 48' 05" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 00:53:43 |
| Azimuth | 57.706° ENE |
| Elevation | -42.833° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 6,085.263 km |
| Perigee | 412.15 km |
| Semi-major axis | 9,626.843 km |
| Eccentricity | 0.2946507 |
| Inclination | 60.8135° |
| RAAN | 321.3968° |
| Arg. of periapsis | 186.2269° |
| True anomaly | 173.84844° |
| Mean anomaly | 169.2275° |
| Eccentric anomaly | 171.67256° |
| Mean motion | 2.29783 °/min |
| BSTAR | 0.0011147 |
| Period | 156.67 mins |
No data available
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. |
|---|---|---|---|---|---|---|---|
| 34 mins | 2024-10-18 07:55:17.527Z | 281.764° WNW | 2024-10-18 08:19:17.527Z | 343.437° N | 29.919° | 2024-10-18 08:29:17.527Z | 43.277° NE |
| 18 mins | 2024-10-18 10:56:17.527Z | 320.311° NNW | 2024-10-18 11:09:17.527Z | 28.676° NE | 32.809° | 2024-10-18 11:14:17.527Z | 90.487° ESE |
| 9 mins | 2024-10-18 13:45:17.527Z | 307.675° NW | 2024-10-18 13:51:17.527Z | 256.889° W | 25.49° | 2024-10-18 13:54:17.527Z | 207.408° SW |
| 54 mins | 2024-10-19 01:37:17.527Z | 168.999° S | 2024-10-19 02:10:17.527Z | 106.467° ESE | 36.578° | 2024-10-19 02:31:17.527Z | 46.275° ENE |
| 55 mins | 2024-10-19 04:20:17.527Z | 220.995° SW | 2024-10-19 04:57:17.527Z | 316.291° NNW | 44.144° | 2024-10-19 05:15:17.527Z | 37.363° NE |