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
Unknown
Mission
Operational Defense Technology
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
4.795 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 OBJECT Q
1 61908U 24205Q 25325.32859539 .00009248 00000-0 46431-3 0 9992
2 61908 97.4386 36.9998 0014066 62.4244 297.8417 15.17427762 56816Epoch: 2025-11-21T07:53Z
TLE epoch observation values (Epoch: 2025-11-21T07:53:10.641Z)
Latitude
0.00001°
Longitude
-141.86773°
Altitude
512.186 km
Speed
7.61 km/s
True Right ascension
02h 27m 59s
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
13:12:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
520.278 km
Perigee altitude
500.899 km
Semi-major axis
6,888.726 km
Eccentricity
0.00141
Inclination
97.4386°
RAAN
36.9998°
Arg. of periapsis
62.4244°
True anomaly
297.69906°
Mean anomaly
297.8417°
Eccentric anomaly
297.77039°
Mean motion
3.79608 °/min
Orbital period
94.83 mins
BSTAR
0.00046431
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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 | 2025-11-23 17:25:12.050Z | 26.651° NE | 2025-11-23 17:28:12.050Z | 81.406° E | 33.928° | 2025-11-23 17:31:12.050Z | 166.541° S |
| 4 mins | 2025-11-24 04:06:12.050Z | 98.179° ESE | 2025-11-24 04:07:12.050Z | 78.716° E | 17.407° | 2025-11-24 04:10:12.050Z | 24.034° NE |
| 4 mins | 2025-11-24 05:40:12.050Z | 230.813° WSW | 2025-11-24 05:41:12.050Z | 255.498° W | 23.191° | 2025-11-24 05:44:12.050Z | 317.969° 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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