OBJECT B, 62726
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 B, 62726 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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62726 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Yinhe
Mission
Operational Civil Imaging
Bus & Motor
TIANLU, Unknown motor
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.475 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 OBJECT B
1 62726U 25012B 25260.78730067 .00004050 00000-0 20457-3 0 9996
2 62726 97.4554 332.8570 0010784 141.5134 218.6871 15.17600955 36883Epoch: 2025-09-17T18:53Z
TLE epoch observation values (Epoch: 2025-09-17T18:53:42.777Z)
Latitude
-0.00002°
Longitude
52.47053°
Altitude
521.984 km
Speed
7.599 km/s
True Right ascension
22h 11m 25s
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
22:18:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
517.493 km
Perigee altitude
502.636 km
Semi-major axis
6,888.202 km
Eccentricity
0.00108
Inclination
97.4554°
RAAN
332.857°
Arg. of periapsis
141.5134°
True anomaly
218.60994°
Mean anomaly
218.6871°
Eccentric anomaly
218.64851°
Mean motion
3.79651 °/min
Orbital period
94.82 mins
BSTAR
0.00020457
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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 B 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 17:37:55.471Z | 24.133° NE | 2025-09-18 17:39:55.471Z | 110.43° ESE | 42.611° | 2025-09-18 17:42:55.471Z | 183.155° SSW |
| 4 mins | 2025-09-19 04:16:55.471Z | 114.125° SE | 2025-09-19 04:18:55.471Z | 66.207° ENE | 24.188° | 2025-09-19 04:20:55.471Z | 23.111° NE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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