OBJECT A, 61238
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, 61238 is a Chinese satellite in SSO that was launched on Tue, 24 Sep 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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61238 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
ZHWK/HITSAT
Mission
Operational Commercial Radar Imaging
Bus & Motor
ZK1, Unknown motor
Mass
~250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 3 Pan, 3.0 m
Radar Cross Section
3.533 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 OBJECT A
1 61238U 24174A 25258.93228110 .00003237 00000-0 15729-3 0 9998
2 61238 97.4533 265.4476 0001663 88.5505 271.5920 15.19145930 54041Epoch: 2025-09-15T22:22Z
TLE epoch observation values (Epoch: 2025-09-15T22:22:29.087Z)
Latitude
0°
Longitude
-65.30344°
Altitude
511.477 km
Speed
7.608 km/s
True Right ascension
17h 41m 47s
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
23:22:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.534 km
Perigee altitude
504.245 km
Semi-major axis
6,883.527 km
Eccentricity
0.00017
Inclination
97.4533°
RAAN
265.4476°
Arg. of periapsis
88.5505°
True anomaly
271.57295°
Mean anomaly
271.592°
Eccentric anomaly
271.58248°
Mean motion
3.80038 °/min
Orbital period
94.73 mins
BSTAR
0.00015729
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Other satellites on launch #174 in the year 2024 (2024-09-24 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-16 13:09:44.737Z | 21.362° NNE | 2025-09-16 13:12:44.737Z | 77.259° E | 39.552° | 2025-09-16 13:15:44.737Z | 176.773° S |
| 4 mins | 2025-09-16 23:49:44.737Z | 105.714° ESE | 2025-09-16 23:51:44.737Z | 59.158° ENE | 21.071° | 2025-09-16 23:53:44.737Z | 22.283° NNE |
| 4 mins | 2025-09-17 01:23:44.737Z | 234.505° WSW | 2025-09-17 01:24:44.737Z | 255.347° W | 19.175° | 2025-09-17 01:27:44.737Z | 312.712° 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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