OBJECT E, 57008 (Decayed)
Orbit data source: Space-Track
OBJECT E, 57008 was a Chinese satellite in LEO that was launched on Thu, 15 Jun 2023 UTC via a CHANG ZHENG 2D launch vehicle from the Taiyaun Space Center, China (TSC). 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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57008 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 5 months ago
TLE from 5 months ago
0 OBJECT E
1 57008U 23085E 26027.28316359 .08885833 25048-5 13813-2 0 9997
2 57008 97.4485 154.8921 0008178 295.9864 64.0589 16.33973218146316Epoch: 2026-01-27T06:47Z
TLE epoch observation values (Epoch: 2026-01-27T06:47:45.334Z)
Latitude
-0.00003°
Longitude
-73.61358°
Altitude
182.782 km
Speed
7.798 km/s
True Right ascension
10h 19m 34s
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
21:27:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
184.064 km
Perigee altitude
173.339 km
Semi-major axis
6,556.838 km
Eccentricity
0.00082
Inclination
97.4485°
RAAN
154.8921°
Arg. of periapsis
295.9864°
True anomaly
64.14321°
Mean anomaly
64.0589°
Eccentric anomaly
64.10105°
Mean motion
4.08791 °/min
Orbital period
88.06 mins
BSTAR
0.0013813
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Other satellites on launch #85 in the year 2023 (2023-06-15 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
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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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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