OBJECT H, 63298
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 H, 63298 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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63298 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 H
1 63298U 25055H 25256.34178755 .00014509 00000-0 73979-3 0 9992
2 63298 97.6207 31.4887 0010463 35.5902 324.6026 15.16814046 27198Epoch: 2025-09-13T08:12Z
TLE epoch observation values (Epoch: 2025-09-13T08:12:10.444Z)
Latitude
-0.00008°
Longitude
-84.13134°
Altitude
512.678 km
Speed
7.611 km/s
True Right ascension
02h 05m 57s
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
10:37:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
519.666 km
Perigee altitude
505.247 km
Semi-major axis
6,890.593 km
Eccentricity
0.00105
Inclination
97.6207°
RAAN
31.4887°
Arg. of periapsis
35.5902°
True anomaly
324.53308°
Mean anomaly
324.6026°
Eccentric anomaly
324.56785°
Mean motion
3.79453 °/min
Orbital period
94.87 mins
BSTAR
0.00073979
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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 H 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 | 2025-09-13 21:26:04.449Z | 34.251° NE | 2025-09-13 21:29:04.449Z | 93.103° ESE | 28.297° | 2025-09-13 21:32:04.449Z | 158.85° S |
| 5 mins | 2025-09-14 09:40:04.449Z | 205.943° SW | 2025-09-14 09:42:04.449Z | 250.638° W | 28.121° | 2025-09-14 09:45:04.449Z | 322.331° NNW |
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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