ELEKTRO-L 2, 41105
Orbit data source: Space-Track
ELEKTRO-L 2, 41105 is a Commonwealth of Independent States-origin payload satellite in GEO that was launched on Fri, 11 Dec 2015 UTC via a ZENIT-3SLBF 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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41105 intel report (Beta)
ELEKTRO-L 2 details
Identifier | |
Orbit | GEO |
Last TLE update | 10 hours ago |
Origin | |
Manufacturer | Lavochkin |
Mission | Operational Civil Weather |
Bus & Motor | NAVIGATOR, Unknown motor |
Mass | 1,855 kg wet, 1,591 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Box + 1 Pan + 1 Ant, 10 m |
Radar Cross Section | 11.105 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 ELEKTRO-L 2
1 41105U 15074A 24361.09783234 -.00000093 00000-0 00000-0 0 9993
2 41105 5.3311 77.1458 0003859 199.1820 199.4915 1.00271321 33116
Epoch: 2024-12-26T02:20Z
Definitive object data (Epoch: 2024-12-26T02:20:52.714Z)
Latitude | 3.35075° |
Longitude | -14.62188° |
Altitude | 35,801.26 km |
Speed | 3.074 km/s |
True Right ascension | 07h 42m 43s |
True Declination | 3° 20' 51" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -1.33427° |
Longitude | 141.03191° |
Altitude | 35,770.13 km |
Speed | 3.076 km/s |
Apparent Right ascension | 18h 31m 49s |
Apparent Declination | -6° 46' 58" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 12:03:03 |
Azimuth | 90.627° ESE |
Elevation | -9.856° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 35,804.054 km |
Perigee altitude | 35,771.51 km |
Semi-major axis | 42,165.919 km |
Eccentricity | 0.0003859 |
Inclination | 5.3311° |
RAAN | 77.1458° |
Arg. of periapsis | 199.182° |
True anomaly | 199.47675° |
Mean anomaly | 199.4915° |
Eccentric anomaly | 199.48413° |
Mean motion | 0.25067 °/min |
BSTAR | Unknown |
Orbital period | 1436.16 mins |
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41105 neighbors
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Other satellites on launch #74 in the year 2015 (2015-12-11 UTC)
ELEKTRO-L 2 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. |
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