ELEKTRON 1, 746
Orbit data source: Space-Track
ELEKTRON 1, 746 is a payload satellite owned by OKB-1 (CIS) in HEO that was launched on Thu, 30 Jan 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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746 intel report (Beta)
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ELEKTRON 1 details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 8 hours ago |
| Origin | |
| Manufacturer | OKB-1 |
| Mission | Civil Science |
| Bus & Motor | OBJECT D, SRM |
| 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 8 hours ago
0 ELEKTRON 1
1 00746U 64006A 24291.91676811 .00003190 00000-0 78977-3 0 9994
2 00746 60.8617 290.5644 3018079 71.8345 318.4972 9.08156740 11997Epoch: 2024-10-17T22:00Z
Definitive object data (Epoch: 2024-10-17T22:00:08.764Z)
| Latitude | -0.00006° |
| Longitude | -66.36613° |
| Altitude | 1,681.109 km |
| Speed | 7.607 km/s |
| True Right ascension | 19h 22m 15s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | -41.88242° |
| Longitude | -96.66446° |
| Altitude | 4,111.66 km |
| Speed | 5.915 km/s |
| Apparent Right ascension | 15h 31m 47s |
| Apparent Declination | -47° 04' 12" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 00:23:27 |
| Azimuth | 242.111° WSW |
| Elevation | -55.643° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 6,253.936 km |
| Perigee | 396.759 km |
| Semi-major axis | 9,703.485 km |
| Eccentricity | 0.3018079 |
| Inclination | 60.8617° |
| RAAN | 290.5644° |
| Arg. of periapsis | 71.8345° |
| True anomaly | 288.2604° |
| Mean anomaly | 318.4972° |
| Eccentric anomaly | 304.19405° |
| Mean motion | 2.27066 °/min |
| BSTAR | 0.00078977 |
| Period | 158.54 mins |
No data available
No data available
Other satellites on launch #6 in the year 1964 (1964-01-30 UTC)
ELEKTRON 1 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2024-10-18 09:01:06.175Z | 353.141° N | 2024-10-18 09:05:06.175Z | 53.947° ENE | 24.609° | 2024-10-18 09:12:06.175Z | 103.726° ESE |
| 18 mins | 2024-10-18 11:44:06.175Z | 295.771° NW | 2024-10-18 11:49:06.175Z | 230.483° WSW | 34.335° | 2024-10-18 12:02:06.175Z | 171.011° S |