OBJECT M, 61905
Orbit data source: Space-Track
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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 | 11 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 11 hours ago
0 OBJECT M
1 61905U 24205M 24348.44635408 .00007862 00000-0 42029-3 0 9992
2 61905 97.4753 60.0827 0015041 170.2922 189.8604 15.15256634 4856Epoch: 2024-12-13T10:42Z
Definitive object data (Epoch: 2024-12-13T10:42:44.992Z)
| Latitude | -0.00002° |
| Longitude | 176.78302° |
| Altitude | 533.507 km |
| Speed | 7.59 km/s |
| True Right ascension | 04h 00m 19s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -3.6579° |
| Longitude | 177.71501° |
| Altitude | 534.09 km |
| Speed | 7.59 km/s |
| Apparent Right ascension | 05h 47m 33s |
| Apparent Declination | -24° 07' 09" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 20:19:13 |
| Azimuth | 75.162° E |
| Elevation | -54.533° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 527.546 km |
| Perigee altitude | 506.803 km |
| Semi-major axis | 6,895.312 km |
| Eccentricity | 0.0015041 |
| Inclination | 97.4753° |
| RAAN | 60.0827° |
| Arg. of periapsis | 170.2922° |
| True anomaly | 189.83094° |
| Mean anomaly | 189.8604° |
| Eccentric anomaly | 189.84566° |
| Mean motion | 3.79064 °/min |
| BSTAR | 0.00042029 |
| Orbital period | 94.97 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-14 04:17:26.095Z | 120.247° SE | 2024-12-14 04:20:26.095Z | 60.568° ENE | 21.914° | 2024-12-14 04:22:26.095Z | 22.934° NE |
| 4 mins | 2024-12-14 05:52:26.095Z | 229.922° WSW | 2024-12-14 05:54:26.095Z | 272.017° WNW | 19.767° | 2024-12-14 05:56:26.095Z | 308.794° NW |
| 5 mins | 2024-12-14 17:24:26.095Z | 40.361° NE | 2024-12-14 17:26:26.095Z | 89.257° E | 30.282° | 2024-12-14 17:29:26.095Z | 161.426° S |
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