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 satellite owned by Zhongke Xiguang (CN) 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
XIOPM/ZXHK
Mission
Operational Commercial Imaging
Bus & Motor
MN100?, Unknown motor
Mass
~75 kg wet, ~75 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: 18 hours ago
TLE from 18 hours ago
0 OBJECT N
1 61906U 24205N 25261.31868667 .00012362 00000-0 48873-3 0 9993
2 61906 97.4445 336.2824 0009860 281.8405 78.1727 15.25581080 47251Epoch: 2025-09-18T07:38Z
TLE epoch observation values (Epoch: 2025-09-18T07:38:54.528Z)
Latitude
-0.00001°
Longitude
-135.9268°
Altitude
490.756 km
Speed
7.62 km/s
True Right ascension
22h 25m 07s
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
18:27:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
492.769 km
Perigee altitude
479.233 km
Semi-major axis
6,864.138 km
Eccentricity
0.00099
Inclination
97.4445°
RAAN
336.2824°
Arg. of periapsis
281.8405°
True anomaly
78.28332°
Mean anomaly
78.1727°
Eccentric anomaly
78.22801°
Mean motion
3.81649 °/min
Orbital period
94.33 mins
BSTAR
0.00048873
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-19 04:16:17.758Z | 104.048° ESE | 2025-09-19 04:18:17.758Z | 63.959° ENE | 17.646° | 2025-09-19 04:20:17.758Z | 27.64° NE |
| 4 mins | 2025-09-19 05:50:17.758Z | 234.471° WSW | 2025-09-19 05:51:17.758Z | 260.15° W | 22.746° | 2025-09-19 05:54:17.758Z | 319.441° NNW |
| 4 mins | 2025-09-19 17:18:17.758Z | 68.626° E | 2025-09-19 17:19:17.758Z | 94.395° ESE | 22.487° | 2025-09-19 17:22:17.758Z | 151.825° SSE |
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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