H-2A DEB, 57802
Orbit data source: Space-Track
H-2A DEB, 57802 is space debris in LEO originally from a launch on Wed, 06 Sep 2023 UTC launched from the Tanegashima Space Center (TNSTA). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
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57802 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Last TLE update
23 hours ago
Origin
Manufacturer
MHI Tobishima
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~200 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Half Cyl, 4 m
Radar Cross Section
13.425 m², Large (>1 m²)
Expand to show TLE details & history
TLE from 23 hours ago
0 H-2A DEB
1 57802U 23137C 25196.59311619 .00077026 00000-0 14260-2 0 9993
2 57802 30.9947 295.4146 0002580 286.0323 74.0041 15.47666610102793Epoch: 2025-07-15T14:14Z
TLE epoch observation values (Epoch: 2025-07-15T14:14:05.238Z)
Latitude
-0.00004°
Longitude
148.2073°
Altitude
421.555 km
Speed
7.661 km/s
True Right ascension
19h 41m 39s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
6.27587°
Longitude
152.06944°
Altitude
420.587 km
Speed
7.662 km/s
Apparent Right ascension
17h 37m 14s
Apparent Declination
-21° 19' 18"
Sunlit
Visualization observer readout
Local Sidereal Time
02:08:14
Azimuth
276.743° WNW
Elevation
-42.125°
Doppler factor
1
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Other satellites on launch #137 in the year 2023 (2023-09-06 UTC)
H-2A DEB Visibility
Observer location: undefined°, undefined°
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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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Authenticating...
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