OBJECT D, 53387 (Decayed)
Orbit data source: Space-Track
OBJECT D, 53387 was a satellite owned by Xinghe Dongli (CN) in LEO that was launched on Tue, 09 Aug 2022 UTC launched 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. This object's orbit decayed before it could be identified.
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53387 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Xinghe Dongli
Mission
Decayed spacecraft
Bus & Motor
EDGE, EDGE
Mass
~150 kg wet, ~150 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Unknown
Shape & HBR
Cyl, 0.6 m
Radar Cross Section
1.602 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year ago
0 OBJECT D
1 53387U 22095D 25034.31389506 .22620994 27936-5 20653-3 0 9998
2 53387 97.2782 133.4632 0006618 217.2595 217.2620 16.51636382140182Epoch: 2025-02-03T07:32Z
TLE epoch observation values (Epoch: 2025-02-03T07:32:00.533Z)
Latitude
72.96734°
Longitude
-137.76137°
Altitude
151.036 km
Speed
7.82 km/s
True Right ascension
07h 15m 54s
True Declination
72° 51' 42"
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
21:35:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
136.125 km
Perigee altitude
127.509 km
Semi-major axis
6,509.954 km
Eccentricity
0.00066
Inclination
97.2782°
RAAN
133.4632°
Arg. of periapsis
217.2595°
True anomaly
217.21611°
Mean anomaly
217.262°
Eccentric anomaly
217.23905°
Mean motion
4.13215 °/min
Orbital period
87.12 mins
BSTAR
0.00020653
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Other satellites on launch #95 in the year 2022 (2022-08-09 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
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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. |
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| This satellite is decayed. |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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