OBJECT M, 61905
Orbit data source: Space-Track
You're viewing an Uncataloged Satellite
Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.
OBJECT M, 61905 is a Chinese satellite in SSO that was launched on Wed, 13 Nov 2024 UTC via a LIJIAN-1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity.
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61905 intel report (Beta)
OBJECT M details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 3 hours ago |
| Origin | |
| Manufacturer | XIOPM/ZXHK |
| Mission | Operational spacecraft |
| Bus & Motor | MN100?, Unknown motor |
| Mass | 75 kg wet, 75 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Unknown |
| Shape & HBR | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 3 hours ago
0 OBJECT M
1 61905U 24205M 24326.13252466 .00008571 00000-0 46462-3 0 9996
2 61905 97.4748 38.1455 0014178 251.2032 168.0924 15.14742002 1472Epoch: 2024-11-21T03:10Z
Definitive object data (Epoch: 2024-11-21T03:10:50.13Z)
| Latitude | 58.61919° |
| Longitude | -82.53486° |
| Altitude | 541.28 km |
| Speed | 7.592 km/s |
| True Right ascension | 01h 43m 10s |
| True Declination | 58° 27' 41" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 82.54373° |
| Longitude | -164.47018° |
| Altitude | 544.51 km |
| Speed | 7.592 km/s |
| Apparent Right ascension | 16h 09m 08s |
| Apparent Declination | 27° 46' 20" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 03:31:54 |
| Azimuth | 351.135° N |
| Elevation | -21.759° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 528.516 km |
| Perigee altitude | 508.959 km |
| Semi-major axis | 6,896.875 km |
| Eccentricity | 0.0014178 |
| Inclination | 97.4748° |
| RAAN | 38.1455° |
| Arg. of periapsis | 251.2032° |
| True anomaly | 168.12586° |
| Mean anomaly | 168.0924° |
| Eccentric anomaly | 168.10914° |
| Mean motion | 3.78935 °/min |
| BSTAR | 0.00046462 |
| Orbital period | 95 mins |
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Other satellites on launch #205 in the year 2024 (2024-11-13 UTC)
OBJECT M 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-11-21 17:45:22.056Z | 17.914° NNE | 2024-11-21 17:48:22.056Z | 108.102° ESE | 43.566° | 2024-11-21 17:51:22.056Z | 185.085° SSW |
| 5 mins | 2024-11-22 04:26:22.056Z | 118.446° SE | 2024-11-22 04:28:22.056Z | 69.856° E | 26.511° | 2024-11-22 04:31:22.056Z | 12.257° NNE |
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