OBJECT D, 62732
Orbit data source: Space-Track
OBJECT D, 62732 is a Chinese payload satellite in SSO that was launched on Mon, 20 Jan 2025 UTC via a GUSHENXING 1 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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62732 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Unknown
Mission
Operational Commercial Meteo Radio Occ.
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 2.5 m
Radar Cross Section
5.339 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 OBJECT D
1 62732U 25013D 26318.93281685 .00003624 00000-0 21381-3 0 9996
2 62732 97.6646 128.7145 0007238 226.3129 133.7502 15.12178209100056Epoch: 2026-11-14T22:23Z
TLE epoch observation values (Epoch: 2026-11-14T22:23:15.375Z)
Latitude
-0.00005°
Longitude
98.86994°
Altitude
536.091 km
Speed
7.593 km/s
True Right ascension
08h 34m 51s
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
02:20:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
531.544 km
Perigee altitude
521.548 km
Semi-major axis
6,904.683 km
Eccentricity
0.00072
Inclination
97.6646°
RAAN
128.7145°
Arg. of periapsis
226.3129°
True anomaly
133.81008°
Mean anomaly
133.7502°
Eccentric anomaly
133.78014°
Mean motion
3.78292 °/min
Orbital period
95.16 mins
BSTAR
0.00021381
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Other satellites on launch #13 in the year 2025 (2025-01-20 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 D 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 | 2026-11-15 11:13:31.554Z | 147.825° SSE | 2026-11-15 11:16:31.554Z | 66.154° ENE | 53.366° | 2026-11-15 11:19:31.554Z | 359.898° N |
| 6 mins | 2026-11-16 00:22:31.554Z | 12.617° NNE | 2026-11-16 00:24:31.554Z | 14.257° NNE | 74.948° | 2026-11-16 00:28:31.554Z | 193.219° SSW |
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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