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: 17 hours ago
TLE from 17 hours ago
0 OBJECT Q
1 61908U 24205Q 25259.63651213 .00007342 00000-0 37587-3 0 9996
2 61908 97.4454 332.4941 0012159 288.1626 71.8283 15.16843304 46853Epoch: 2025-09-16T15:16Z
TLE epoch observation values (Epoch: 2025-09-16T15:16:34.648Z)
Latitude
-0.00001°
Longitude
107.52577°
Altitude
515.868 km
Speed
7.607 km/s
True Right ascension
22h 09m 58s
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
00:57:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.738 km
Perigee altitude
503.982 km
Semi-major axis
6,890.497 km
Eccentricity
0.00122
Inclination
97.4454°
RAAN
332.4941°
Arg. of periapsis
288.1626°
True anomaly
71.96075°
Mean anomaly
71.8283°
Eccentric anomaly
71.89452°
Mean motion
3.79461 °/min
Orbital period
94.87 mins
BSTAR
0.00037587
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-17 17:10:25.858Z | 36.186° NE | 2025-09-17 17:13:25.858Z | 88.927° E | 24.892° | 2025-09-17 17:16:25.858Z | 152.173° SSE |
| 5 mins | 2025-09-18 05:24:25.858Z | 198.211° SSW | 2025-09-18 05:26:25.858Z | 244.356° WSW | 32.692° | 2025-09-18 05:29:25.858Z | 326.842° NNW |
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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