OBJECT E, 51828
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 E, 51828 is a satellite owned by Sanya RI (CN) in SSO that was launched on Sun, 27 Feb 2022 UTC via a CHANG ZHENG 8 launch vehicle from the Wenchang Satellite Launch Center (WSC). 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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51828 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
None
Manufacturer
Weina
Mission
Civil Imaging
Bus & Motor
MN50?, Unknown motor
Mass
62 kg wet, 62 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Unknown
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
1.775 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 OBJECT E
1 51828U 22019E 25256.31535215 .00011978 00000-0 25434-3 0 9990
2 51828 97.3922 340.8585 0008991 49.5093 310.6938 15.45139138197049Epoch: 2025-09-13T07:34Z
TLE epoch observation values (Epoch: 2025-09-13T07:34:06.425Z)
Latitude
-0.00003°
Longitude
-125.21874°
Altitude
430.105 km
Speed
7.656 km/s
True Right ascension
22h 43m 26s
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
18:15:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
434.02 km
Perigee altitude
421.782 km
Semi-major axis
6,806.038 km
Eccentricity
0.0009
Inclination
97.3922°
RAAN
340.8585°
Arg. of periapsis
49.5093°
True anomaly
310.61563°
Mean anomaly
310.6938°
Eccentric anomaly
310.65472°
Mean motion
3.86546 °/min
Orbital period
93.13 mins
BSTAR
0.00025434
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Other satellites on launch #19 in the year 2022 (2022-02-27 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 E 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 | 2025-09-14 05:27:43.617Z | 145.195° SSE | 2025-09-14 05:30:43.617Z | 49.422° ENE | 33.628° | 2025-09-14 05:32:43.617Z | 5.154° NNE |
| 4 mins | 2025-09-14 18:20:43.617Z | 42.462° NE | 2025-09-14 18:21:43.617Z | 81.922° E | 36.023° | 2025-09-14 18:24:43.617Z | 173.718° S |
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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