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 Mon, 11 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)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.8 m
Radar Cross Section
2.000 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 OBJECT M
1 61905U 24205M 25317.85019149 .00031700 00000-0 14970-2 0 9993
2 61905 97.4388 29.2290 0020523 143.9067 216.3558 15.19176386 55656Epoch: 2025-11-13T20:24Z
TLE epoch observation values (Epoch: 2025-11-13T20:24:16.544Z)
Latitude
-0°
Longitude
29.95794°
Altitude
522.812 km
Speed
7.596 km/s
True Right ascension
01h 56m 54s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:41:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.424 km
Perigee altitude
491.17 km
Semi-major axis
6,883.434 km
Eccentricity
0.00205
Inclination
97.4388°
RAAN
29.229°
Arg. of periapsis
143.9067°
True anomaly
216.21668°
Mean anomaly
216.3558°
Eccentric anomaly
216.28621°
Mean motion
3.80045 °/min
Orbital period
94.73 mins
BSTAR
0.001497
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Other satellites on launch #205 in the year 2024 (2024-11-11 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OBJECT M Visibility forecast
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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 | 2025-11-14 17:30:50.040Z | 22.183° NNE | 2025-11-14 17:33:50.040Z | 76.205° E | 38.085° | 2025-11-14 17:36:50.040Z | 174.674° S |
| 4 mins | 2025-11-15 04:10:50.040Z | 105.675° ESE | 2025-11-15 04:12:50.040Z | 61.064° ENE | 20.468° | 2025-11-15 04:14:50.040Z | 23.931° NE |
| 4 mins | 2025-11-15 05:44:50.040Z | 232.531° WSW | 2025-11-15 05:45:50.040Z | 253.664° W | 20.013° | 2025-11-15 05:48:50.040Z | 312.967° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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