OBJECT Q, 61908
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 Q, 61908 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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61908 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
STARV/SQU
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 0.5 m
Radar Cross Section
0.195 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 OBJECT Q
1 61908U 24205Q 25252.31380233 .00005836 00000-0 30027-3 0 9993
2 61908 97.4465 325.3039 0012443 316.7516 43.2740 15.16753577 45746Epoch: 2025-09-09T07:31Z
TLE epoch observation values (Epoch: 2025-09-09T07:31:52.521Z)
Latitude
0.00005°
Longitude
-136.2713°
Altitude
512.503 km
Speed
7.611 km/s
True Right ascension
21h 41m 12s
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
19:34:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
521.206 km
Perigee altitude
504.058 km
Semi-major axis
6,890.769 km
Eccentricity
0.00124
Inclination
97.4465°
RAAN
325.3039°
Arg. of periapsis
316.7516°
True anomaly
43.37185°
Mean anomaly
43.274°
Eccentric anomaly
43.32291°
Mean motion
3.79439 °/min
Orbital period
94.88 mins
BSTAR
0.00030027
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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 Q 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-10 04:15:26.976Z | 121.247° SE | 2025-09-10 04:18:26.976Z | 60.733° ENE | 22.052° | 2025-09-10 04:20:26.976Z | 22.54° NE |
| 4 mins | 2025-09-10 05:50:26.976Z | 231.621° WSW | 2025-09-10 05:52:26.976Z | 273.615° WNW | 18.875° | 2025-09-10 05:54:26.976Z | 309.354° NW |
| 5 mins | 2025-09-10 17:22:26.976Z | 50.48° ENE | 2025-09-10 17:24:26.976Z | 116.49° SE | 30.291° | 2025-09-10 17:27:26.976Z | 166.777° S |
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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