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). 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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Edit Public Description
| Identifier | |
| Orbit | Active |
| Last TLE update | 13 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 13 hours ago
0 ELEKTRON 3
1 00829U 64038A 25081.49006357 .00003886 00000-0 10282-2 0 9990
2 00829 60.8152 105.9629 2948202 227.9540 103.0260 9.20001414973856Epoch: 2025-03-22T11:45Z
Definitive object data (Epoch: 2025-03-22T11:45:41.492Z)
| Latitude | -0.00002° |
| Longitude | 109.30562° |
| Altitude | 4,572.911 km |
| Speed | 5.602 km/s |
| True Right ascension | 07h 03m 51s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 34.01682° |
| Longitude | 130.60443° |
| Altitude | 6,027.239 km |
| Speed | 4.782 km/s |
| Apparent Right ascension | 10h 02m 00s |
| Apparent Declination | 23° 00' 00" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 06:18:07 |
| Azimuth | 92.315° ESE |
| Elevation | 40.226° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 6,078.055 km |
| Perigee altitude | 405.705 km |
| Semi-major axis | 9,620.017 km |
| Eccentricity | 0.2948202 |
| Inclination | 60.8152° |
| RAAN | 105.9629° |
| Arg. of periapsis | 227.954° |
| True anomaly | 132.129° |
| Mean anomaly | 103.026° |
| Eccentric anomaly | 117.94791° |
| Mean motion | 2.30027 °/min |
| BSTAR | 0.0010282 |
| Orbital period | 156.5 mins |
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Other satellites on launch #38 in the year 1964 (1964-07-10 UTC)
| 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: undefined°, undefined°
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. |
|---|---|---|---|---|---|---|---|
| 28 mins | 2025-03-23 01:15:26.759Z | 92.423° ESE | 2025-03-23 01:15:26.759Z | 92.423° ESE | 32.839° | 2025-03-23 01:43:26.759Z | 42.387° NE |
| 66 mins | 2025-03-23 03:26:26.759Z | 212.282° SW | 2025-03-23 03:58:26.759Z | 302.966° NW | 44.958° | 2025-03-23 04:32:26.759Z | 40.518° NE |
| 61 mins | 2025-03-23 06:18:26.759Z | 264.733° W | 2025-03-23 06:54:26.759Z | 337.153° NNW | 37.617° | 2025-03-23 07:19:26.759Z | 54.637° ENE |
| 44 mins | 2025-03-23 09:22:26.759Z | 307.41° NW | 2025-03-23 09:53:26.759Z | 21.918° NNE | 37.778° | 2025-03-23 10:06:26.759Z | 93.044° ESE |
| 31 mins | 2025-03-23 12:18:26.759Z | 320.525° NNW | 2025-03-23 12:40:26.759Z | 250.274° W | 43.081° | 2025-03-23 12:49:26.759Z | 163.88° S |
| 52 mins | 2025-03-24 00:18:26.759Z | 143.564° SSE | 2025-03-24 00:42:26.759Z | 92.281° ESE | 29.098° | 2025-03-24 01:10:26.759Z | 43.262° NE |
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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