OBJECT G, 63297
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, 63297 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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63297 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
ZHWK/HITSAT
Mission
Operational Commercial Imaging
Bus & Motor
ZK1, Unknown motor
Mass
~250 kg wet, ~250 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 3 Pan, 3.0 m
Radar Cross Section
3.533 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT G
1 63297U 25055G 25256.34921493 .00008412 00000-0 45951-3 0 9991
2 63297 97.6214 31.1850 0010933 40.2500 319.9539 15.14519917 27172Epoch: 2025-09-13T08:22Z
TLE epoch observation values (Epoch: 2025-09-13T08:22:52.169Z)
Latitude
-0.00006°
Longitude
-87.11621°
Altitude
519.74 km
Speed
7.607 km/s
True Right ascension
02h 04m 44s
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
10:39:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.96 km
Perigee altitude
511.878 km
Semi-major axis
6,897.556 km
Eccentricity
0.00109
Inclination
97.6214°
RAAN
31.185°
Arg. of periapsis
40.25°
True anomaly
319.87321°
Mean anomaly
319.9539°
Eccentric anomaly
319.91356°
Mean motion
3.78879 °/min
Orbital period
95.02 mins
BSTAR
0.00045951
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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 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-13 21:37:34.208Z | 24.701° NE | 2025-09-13 21:40:34.208Z | 75.772° E | 35.763° | 2025-09-13 21:44:34.208Z | 175.225° S |
| 4 mins | 2025-09-14 08:19:34.208Z | 105.454° ESE | 2025-09-14 08:21:34.208Z | 61.842° ENE | 20.308° | 2025-09-14 08:23:34.208Z | 24.598° NE |
| 4 mins | 2025-09-14 09:53:34.208Z | 226.587° WSW | 2025-09-14 09:55:34.208Z | 270.447° WNW | 20.795° | 2025-09-14 09:57:34.208Z | 309.298° NW |
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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