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: 5 hours ago
TLE from 5 hours ago
0 OBJECT N
1 61906U 24205N 26004.87977090 .00023321 00000-0 78273-3 0 9995
2 61906 97.4328 84.6625 0008970 257.1045 102.9194 15.30837064 63839Epoch: 2026-01-04T21:06Z
TLE epoch observation values (Epoch: 2026-01-04T21:06:52.205Z)
Latitude
-0.00006°
Longitude
23.46004°
Altitude
477.797 km
Speed
7.626 km/s
True Right ascension
05h 38m 39s
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
02:27:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
476.409 km
Perigee altitude
464.123 km
Semi-major axis
6,848.403 km
Eccentricity
0.0009
Inclination
97.4328°
RAAN
84.6625°
Arg. of periapsis
257.1045°
True anomaly
103.01956°
Mean anomaly
102.9194°
Eccentric anomaly
102.96948°
Mean motion
3.82965 °/min
Orbital period
94 mins
BSTAR
0.00078273
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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 | 2026-01-05 05:04:49.076Z | 158.989° S | 2026-01-05 05:07:49.076Z | 113.11° SE | 42.026° | 2026-01-05 05:10:49.076Z | 354.901° N |
| 5 mins | 2026-01-05 18:04:49.076Z | 11.266° NNE | 2026-01-05 18:06:49.076Z | 2.361° NNE | 44.374° | 2026-01-05 18:09:49.076Z | 193.837° 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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