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 Chinese satellite 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
Unknown
Mission
Civil Imaging
Bus & Motor
Unknown
Mass
Unknown
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: 19 hours ago
TLE from 19 hours ago
0 OBJECT E
1 51828U 22019E 25348.98135652 .00016033 00000-0 28845-3 0 9992
2 51828 97.3874 75.4807 0008397 66.5788 293.6346 15.49880364211377Epoch: 2025-12-14T23:33Z
TLE epoch observation values (Epoch: 2025-12-14T23:33:09.203Z)
Latitude
0.00004°
Longitude
-1.69413°
Altitude
417.923 km
Speed
7.662 km/s
True Right ascension
05h 01m 55s
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
17:10:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
419.704 km
Perigee altitude
408.298 km
Semi-major axis
6,792.138 km
Eccentricity
0.00084
Inclination
97.3874°
RAAN
75.4807°
Arg. of periapsis
66.5788°
True anomaly
293.54641°
Mean anomaly
293.6346°
Eccentric anomaly
293.59051°
Mean motion
3.87734 °/min
Orbital period
92.85 mins
BSTAR
0.00028845
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-15 18:41:56.519Z | 17.309° NNE | 2025-12-15 18:44:56.519Z | 114.082° SE | 43.008° | 2025-12-15 18:47:56.519Z | 185.596° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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