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
Unknown
Mission
Operational Commercial Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 3 Pan, 0.5 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 25359.34006270 .00031502 00000-0 12969-2 0 9991
2 63298 97.6282 135.6521 0009181 36.0292 324.1561 15.24025226 42847Epoch: 2025-12-25T08:09Z
TLE epoch observation values (Epoch: 2025-12-25T08:09:41.417Z)
Latitude
-0.00009°
Longitude
-80.86697°
Altitude
491.69 km
Speed
7.622 km/s
True Right ascension
09h 02m 36s
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
17:54:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
496.99 km
Perigee altitude
484.378 km
Semi-major axis
6,868.821 km
Eccentricity
0.00092
Inclination
97.6282°
RAAN
135.6521°
Arg. of periapsis
36.0292°
True anomaly
324.09444°
Mean anomaly
324.1561°
Eccentric anomaly
324.12527°
Mean motion
3.81259 °/min
Orbital period
94.42 mins
BSTAR
0.0012969
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-12-25 21:20:51.702Z | 52.818° ENE | 2025-12-25 21:22:51.702Z | 90.694° ESE | 18.593° | 2025-12-25 21:24:51.702Z | 131.901° SE |
| 4 mins | 2025-12-25 22:54:51.702Z | 328.756° NNW | 2025-12-25 22:56:51.702Z | 282.367° WNW | 21.451° | 2025-12-25 22:58:51.702Z | 242.963° WSW |
| 5 mins | 2025-12-26 09:30:51.702Z | 184.972° SSW | 2025-12-26 09:32:51.702Z | 262.222° W | 41.23° | 2025-12-26 09:35:51.702Z | 338.994° N |
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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