OBJECT D, 63294
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 D, 63294 is a Chinese satellite in SSO that was launched on Mon, 17 Mar 2025 UTC via a GUSHENXING 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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63294 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, 0.6 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 OBJECT D
1 63294U 25055D 25320.81150699 .00015686 00000-0 91429-3 0 9996
2 63294 97.6281 94.7827 0017302 149.5572 210.6666 15.11946751 36862Epoch: 2025-11-16T19:28Z
TLE epoch observation values (Epoch: 2025-11-16T19:28:34.203Z)
Latitude
-0.00009°
Longitude
106.51926°
Altitude
543.626 km
Speed
7.585 km/s
True Right ascension
06h 19m 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
04:48:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.197 km
Perigee altitude
515.302 km
Semi-major axis
6,905.387 km
Eccentricity
0.00173
Inclination
97.6281°
RAAN
94.7827°
Arg. of periapsis
149.5572°
True anomaly
210.56566°
Mean anomaly
210.6666°
Eccentric anomaly
210.61611°
Mean motion
3.78235 °/min
Orbital period
95.18 mins
BSTAR
0.00091429
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Other satellites on launch #55 in the year 2025 (2025-03-17 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 D 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-17 08:19:59.485Z | 115.175° SE | 2025-11-17 08:21:59.485Z | 78.038° E | 21.298° | 2025-11-17 08:24:59.485Z | 20.323° NNE |
| 4 mins | 2025-11-17 09:54:59.485Z | 230.507° WSW | 2025-11-17 09:56:59.485Z | 274.798° WNW | 20.701° | 2025-11-17 09:58:59.485Z | 310.962° NW |
| 5 mins | 2025-11-17 21:28:59.485Z | 51.317° ENE | 2025-11-17 21:30:59.485Z | 113.629° SE | 29.117° | 2025-11-17 21:33:59.485Z | 165.095° S |
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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