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: 6 hours ago
TLE from 6 hours ago
0 OBJECT G
1 63297U 25055G 25260.97388988 .00011538 00000-0 62666-3 0 9996
2 63297 97.6215 35.8164 0010646 24.9562 335.2182 15.14635238 27877Epoch: 2025-09-17T23:22Z
TLE epoch observation values (Epoch: 2025-09-17T23:22:24.085Z)
Latitude
-0.00006°
Longitude
48.0739°
Altitude
518.493 km
Speed
7.608 km/s
True Right ascension
02h 23m 15s
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
22:18:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
526.411 km
Perigee altitude
511.726 km
Semi-major axis
6,897.205 km
Eccentricity
0.00106
Inclination
97.6215°
RAAN
35.8164°
Arg. of periapsis
24.9562°
True anomaly
335.167°
Mean anomaly
335.2182°
Eccentric anomaly
335.19261°
Mean motion
3.78908 °/min
Orbital period
95.01 mins
BSTAR
0.00062666
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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 | 2025-09-18 09:00:13.113Z | 161.49° S | 2025-09-18 09:04:13.113Z | 24.859° NE | 42.835° | 2025-09-18 09:07:13.113Z | 351.598° N |
| 5 mins | 2025-09-18 22:09:13.113Z | 358.22° N | 2025-09-18 22:11:13.113Z | 256.748° W | 41.859° | 2025-09-18 22:14:13.113Z | 203.406° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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