H-2A DEB, 57802 (Decayed)
Orbit data source: Space-Track
H-2A DEB, 57802 was 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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Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
MHI Tobishima
Mission
Decayed 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, 2.0 m
Radar Cross Section
13.425 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 months ago
TLE from 8 months ago
0 H-2A DEB
1 57802U 23137C 25296.72844389 .07524179 -39476-5 24510-2 0 9991
2 57802 30.9811 314.9919 0002860 136.6932 223.3962 16.24880824118479Epoch: 2025-10-23T17:28Z
TLE epoch observation values (Epoch: 2025-10-23T17:28:57.552Z)
Latitude
-0.00004°
Longitude
20.36851°
Altitude
206.134 km
Speed
7.785 km/s
True Right ascension
20h 59m 58s
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
21:37:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
212.254 km
Perigee altitude
208.485 km
Semi-major axis
6,588.506 km
Eccentricity
0.00029
Inclination
30.9811°
RAAN
314.9919°
Arg. of periapsis
136.6932°
True anomaly
223.37369°
Mean anomaly
223.3962°
Eccentric anomaly
223.38494°
Mean motion
4.05847 °/min
Orbital period
88.7 mins
BSTAR
0.002451
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Other satellites on launch #137 in the year 2023 (2023-09-06 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.H-2A DEB 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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