OBJECT A, 61894
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 A, 61894 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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61894 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 OBJECT A
1 61894U 24205A 25312.49864072 .00018392 00000-0 89615-3 0 9999
2 61894 97.4383 23.3788 0023912 80.4870 279.9065 15.18138930 54836Epoch: 2025-11-08T11:58Z
TLE epoch observation values (Epoch: 2025-11-08T11:58:02.558Z)
Latitude
-0°
Longitude
155.94076°
Altitude
511.756 km
Speed
7.609 km/s
True Right ascension
01h 33m 30s
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
17:40:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
524.902 km
Perigee altitude
491.968 km
Semi-major axis
6,886.572 km
Eccentricity
0.00239
Inclination
97.4383°
RAAN
23.3788°
Arg. of periapsis
80.487°
True anomaly
279.63644°
Mean anomaly
279.9065°
Eccentric anomaly
279.77148°
Mean motion
3.79786 °/min
Orbital period
94.79 mins
BSTAR
0.00089615
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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 A 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-09 03:56:23.026Z | 106.411° ESE | 2025-11-09 03:58:23.026Z | 72.66° E | 15.443° | 2025-11-09 04:00:23.026Z | 35.743° NE |
| 5 mins | 2025-11-09 05:30:23.026Z | 214.072° SW | 2025-11-09 05:32:23.026Z | 264.05° W | 26.196° | 2025-11-09 05:35:23.026Z | 323.94° NNW |
| 4 mins | 2025-11-09 17:02:23.026Z | 69.021° E | 2025-11-09 17:03:23.026Z | 93.426° ESE | 21.609° | 2025-11-09 17:06:23.026Z | 149.607° SSE |
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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