OBJECT Q, 61908
Orbit data source: Space-Track
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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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: 6 hours ago
TLE from 6 hours ago
0 OBJECT Q
1 61908U 24205Q 26053.82896046 .00008343 00000-0 41797-3 0 9995
2 61908 97.4231 128.7580 0013959 97.0240 263.2581 15.17535060 70997Epoch: 2026-02-22T19:53Z
TLE epoch observation values (Epoch: 2026-02-22T19:53:42.183Z)
Latitude
-0.00012°
Longitude
37.60067°
Altitude
517.522 km
Speed
7.604 km/s
True Right ascension
08h 35m 01s
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
05:01:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.878 km
Perigee altitude
500.647 km
Semi-major axis
6,888.4 km
Eccentricity
0.0014
Inclination
97.4231°
RAAN
128.758°
Arg. of periapsis
97.024°
True anomaly
263.09928°
Mean anomaly
263.2581°
Eccentric anomaly
263.17869°
Mean motion
3.79634 °/min
Orbital period
94.83 mins
BSTAR
0.00041797
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-02-23 03:57:42.081Z | 105.916° ESE | 2026-02-23 03:59:42.081Z | 72.727° E | 15.374° | 2026-02-23 04:01:42.081Z | 36.312° NE |
| 5 mins | 2026-02-23 05:31:42.081Z | 212.607° SW | 2026-02-23 05:33:42.081Z | 262.589° W | 27.118° | 2026-02-23 05:36:42.081Z | 324.097° NNW |
| 4 mins | 2026-02-23 17:03:42.081Z | 61.964° ENE | 2026-02-23 17:04:42.081Z | 83.943° E | 20.984° | 2026-02-23 17:07:42.081Z | 145.25° SSE |
| 4 mins | 2026-02-23 18:37:42.081Z | 319.762° NNW | 2026-02-23 18:38:42.081Z | 298.584° NW | 19.289° | 2026-02-23 18:41:42.081Z | 242.461° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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