OBJECT G, 63297
Orbit data source: Space-Track
OBJECT G, 63297 is a Chinese payload 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). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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63297 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 26311.32148597 .00026318 00000-0 91044-3 0 9997
2 63297 97.6639 98.2469 0007614 17.9833 342.1674 15.29844362 91085Epoch: 2026-11-07T07:42Z
TLE epoch observation values (Epoch: 2026-11-07T07:42:56.387Z)
Latitude
-0.00011°
Longitude
-64.01645°
Altitude
474.404 km
Speed
7.631 km/s
True Right ascension
06h 32m 59s
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
14:04:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
478.458 km
Perigee altitude
468.024 km
Semi-major axis
6,851.378 km
Eccentricity
0.00076
Inclination
97.6639°
RAAN
98.2469°
Arg. of periapsis
17.9833°
True anomaly
342.14066°
Mean anomaly
342.1674°
Eccentric anomaly
342.15403°
Mean motion
3.82716 °/min
Orbital period
94.06 mins
BSTAR
0.00091044
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-11-07 22:24:51.273Z | 35.068° NE | 2026-11-07 22:27:51.273Z | 119.861° SE | 35.903° | 2026-11-07 22:29:51.273Z | 162.205° S |
| 4 mins | 2026-11-08 10:32:51.273Z | 220.158° SW | 2026-11-08 10:33:51.273Z | 247.047° WSW | 29.557° | 2026-11-08 10:36:51.273Z | 320.965° NNW |
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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