H-2A DEB, 38345 (Decayed)
Orbit data source: Space-Track
H-2A DEB, 38345 was space debris in LEO originally from a launch on Thu, 17 May 2012 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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38345 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
JP / JPNRelated business
Manufacturer
Kawasaki
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
Cone, 2.0 m
Radar Cross Section
6.654 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 months ago
TLE from 3 months ago
0 H-2A DEB
1 38345U 12025F 25201.28147744 .24444827 30553-5 17411-2 0 9992
2 38345 98.1989 29.7628 0015054 264.9832 206.9714 16.39688214714191Epoch: 2025-07-20T06:45Z
TLE epoch observation values (Epoch: 2025-07-20T06:45:19.650Z)
Latitude
66.80159°
Longitude
-170.3476°
Altitude
186.984 km
Speed
7.795 km/s
True Right ascension
15h 17m 09s
True Declination
66° 39' 57"
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
03:40:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
173.326 km
Perigee altitude
153.63 km
Semi-major axis
6,541.615 km
Eccentricity
0.00151
Inclination
98.1989°
RAAN
29.7628°
Arg. of periapsis
264.9832°
True anomaly
206.89329°
Mean anomaly
206.9714°
Eccentric anomaly
206.93233°
Mean motion
4.10219 °/min
Orbital period
87.76 mins
BSTAR
0.0017411
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Other satellites on launch #25 in the year 2012 (2012-05-17 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
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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