OBJECT C, 62727
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 C, 62727 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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62727 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Shikong Daoyu
Mission
Operational Civil Imaging
Bus & Motor
LANTAN, Unknown motor
Mass
66 kg wet, 66 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.583 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 OBJECT C
1 62727U 25012C 25260.96697090 .00009445 00000-0 43821-3 0 9998
2 62727 97.4564 333.5445 0009802 138.5746 221.6234 15.20214200 36928Epoch: 2025-09-17T23:12Z
TLE epoch observation values (Epoch: 2025-09-17T23:12:26.285Z)
Latitude
-0.00004°
Longitude
-11.70035°
Altitude
513.331 km
Speed
7.604 km/s
True Right ascension
22h 14m 10s
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
22:18:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
508.906 km
Perigee altitude
495.418 km
Semi-major axis
6,880.299 km
Eccentricity
0.00098
Inclination
97.4564°
RAAN
333.5445°
Arg. of periapsis
138.5746°
True anomaly
221.54886°
Mean anomaly
221.6234°
Eccentric anomaly
221.58612°
Mean motion
3.80305 °/min
Orbital period
94.66 mins
BSTAR
0.00043821
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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 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-18 05:39:13.419Z | 211.131° SW | 2025-09-18 05:42:13.419Z | 274.838° WNW | 22.868° | 2025-09-18 05:44:13.419Z | 314.118° NW |
| 4 mins | 2025-09-18 17:10:13.419Z | 51.914° ENE | 2025-09-18 17:12:13.419Z | 99.958° ESE | 23.873° | 2025-09-18 17:14:13.419Z | 144.405° SSE |
| 5 mins | 2025-09-19 05:21:13.419Z | 194.891° SSW | 2025-09-19 05:23:13.419Z | 238.003° WSW | 33.143° | 2025-09-19 05:26:13.419Z | 327.598° 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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