OBJECT A, 62725
Orbit data source: Space-Track
OBJECT A, 62725 is a Chinese satellite in SSO that was launched on Fri, 17 Jan 2025 UTC via a CHANG ZHENG 2D 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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62725 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Civil Imaging
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 2.0 m
Radar Cross Section
6.755 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 OBJECT A
1 62725U 25012A 26170.30158772 .00005321 00000-0 26772-3 0 9999
2 62725 97.4222 242.7204 0004908 243.1116 116.9617 15.17630714 78517Epoch: 2026-06-19T07:14Z
TLE epoch observation values (Epoch: 2026-06-19T07:14:17.179Z)
Latitude
0.00006°
Longitude
-133.38371°
Altitude
517.625 km
Speed
7.604 km/s
True Right ascension
16h 10m 52s
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
03:53:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.354 km
Perigee altitude
506.592 km
Semi-major axis
6,888.11 km
Eccentricity
0.00049
Inclination
97.4222°
RAAN
242.7204°
Arg. of periapsis
243.1116°
True anomaly
117.01181°
Mean anomaly
116.9617°
Eccentric anomaly
116.98676°
Mean motion
3.79658 °/min
Orbital period
94.82 mins
BSTAR
0.00026772
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Other satellites on launch #12 in the year 2025 (2025-01-17 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 A 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 | 2026-06-19 17:17:42.504Z | 28.39° NE | 2026-06-19 17:20:42.504Z | 84.37° E | 32.474° | 2026-06-19 17:23:42.504Z | 164.178° S |
| 5 mins | 2026-06-20 05:31:42.504Z | 214.664° SW | 2026-06-20 05:33:42.504Z | 260.335° W | 25.355° | 2026-06-20 05:36:42.504Z | 321.287° 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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