OBJECT N, 61906
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 N, 61906 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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61906 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 OBJECT N
1 61906U 24205N 25306.54362269 .00018747 00000-0 69147-3 0 9995
2 61906 97.4399 21.3428 0012155 122.6316 237.6098 15.27767851 54159Epoch: 2025-11-02T13:02Z
TLE epoch observation values (Epoch: 2025-11-02T13:02:49.000Z)
Latitude
-0.00002°
Longitude
143.5808°
Altitude
490.062 km
Speed
7.617 km/s
True Right ascension
01h 25m 22s
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
23:21:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.779 km
Perigee altitude
471.108 km
Semi-major axis
6,857.581 km
Eccentricity
0.00122
Inclination
97.4399°
RAAN
21.3428°
Arg. of periapsis
122.6316°
True anomaly
237.49228°
Mean anomaly
237.6098°
Eccentric anomaly
237.55103°
Mean motion
3.82197 °/min
Orbital period
94.19 mins
BSTAR
0.00069147
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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 N 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 | 2025-11-03 04:53:24.272Z | 151.379° SSE | 2025-11-03 04:56:24.272Z | 95.368° ESE | 37.807° | 2025-11-03 04:59:24.272Z | 1.212° NNE |
| 5 mins | 2025-11-03 17:55:24.272Z | 20.865° NNE | 2025-11-03 17:57:24.272Z | 153.56° SSE | 42.483° | 2025-11-03 18:00:24.272Z | 187.467° SSW |
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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