OBJECT G, 61900
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 G, 61900 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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61900 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 OBJECT G
1 61900U 24205G 26032.02853274 .00000126 00000-0 11968-4 0 9991
2 61900 97.4281 106.2240 0019167 256.4058 103.5036 15.08727264 67618Epoch: 2026-02-01T00:41Z
TLE epoch observation values (Epoch: 2026-02-01T00:41:05.228Z)
Latitude
-0.00006°
Longitude
-35.29183°
Altitude
546.283 km
Speed
7.587 km/s
True Right ascension
07h 04m 53s
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
02:59:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
550.324 km
Perigee altitude
523.815 km
Semi-major axis
6,915.207 km
Eccentricity
0.00192
Inclination
97.4281°
RAAN
106.224°
Arg. of periapsis
256.4058°
True anomaly
103.71705°
Mean anomaly
103.5036°
Eccentric anomaly
103.61033°
Mean motion
3.77429 °/min
Orbital period
95.38 mins
BSTAR
0.000011968
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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 G 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 | 2026-02-04 05:13:24.860Z | 193.43° SSW | 2026-02-04 05:15:24.860Z | 239.03° WSW | 35.87° | 2026-02-04 05:19:24.860Z | 335.491° NNW |
| 4 mins | 2026-02-04 18:24:24.860Z | 326.417° NNW | 2026-02-04 18:26:24.860Z | 275.743° WNW | 24.347° | 2026-02-04 18:28:24.860Z | 238.055° 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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