OBJECT C, 64089
Orbit data source: Space-Track
OBJECT C, 64089 is a Chinese satellite in SSO that was launched on Wed, 21 May 2025 UTC via a LIJIAN-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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64089 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
Unknown
Shape & HBR
Box, 1.1 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 OBJECT C
1 64089U 25108C 26171.48561997 .00004206 00000-0 23980-3 0 9996
2 64089 97.4683 245.5494 0009845 34.9925 325.1952 15.13282601 59760Epoch: 2026-06-20T11:39Z
TLE epoch observation values (Epoch: 2026-06-20T11:39:17.565Z)
Latitude
0.00004°
Longitude
162.02665°
Altitude
523.696 km
Speed
7.604 km/s
True Right ascension
16h 22m 11s
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
10:17:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.969 km
Perigee altitude
516.38 km
Semi-major axis
6,901.312 km
Eccentricity
0.00098
Inclination
97.4683°
RAAN
245.5494°
Arg. of periapsis
34.9925°
True anomaly
325.13074°
Mean anomaly
325.1952°
Eccentric anomaly
325.16298°
Mean motion
3.7857 °/min
Orbital period
95.09 mins
BSTAR
0.0002398
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Other satellites on launch #108 in the year 2025 (2025-05-21 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 C 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 | 2026-06-21 05:13:41.819Z | 180.706° SSW | 2026-06-21 05:16:41.819Z | 227.135° WSW | 38.436° | 2026-06-21 05:20:41.819Z | 339.079° N |
| 5 mins | 2026-06-21 18:22:41.819Z | 341.859° N | 2026-06-21 18:24:41.819Z | 293.869° NW | 29.315° | 2026-06-21 18:27:41.819Z | 226.688° WSW |
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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