DECAYED

H-2A DEB, 57805 (Decayed)

Orbit data source: Space-Track

H-2A DEB, 57805 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.

Not visible in the next 10 days
Identifier
57805, 2023-137F
Orbit
Decayed
Last TLE update
7 months ago
Origin
Manufacturer
MHI Tobishima
Mission
Decayed spacecraft
Bus & Motor
Unknown
Mass
~300 kg wet, ~300 kg dry
Launch date (UTC)
2023-09-06 (2 years ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cone, 4 m
Radar Cross Section
6.654 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 7 months ago
0 H-2A DEB
1 57805U 23137F   24335.27093362  .38846667 -40540-5  28079-2 0  9995
2 57805  30.9669 318.9857 0000010 200.7346 247.2610 16.39723255 68351
Epoch: 2024-11-30T06:30Z
TLE epoch observation values (Epoch: 2024-11-30T06:30:08.664Z)
Latitude
31.09197°
Longitude
-120.51584°
Altitude
165.903 km
Speed
7.812 km/s
True Right ascension
03h 06m 35s
True Declination
30° 55' 35"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Visualization observer readout
Orbital elements
Apogee altitude
170.608 km
Perigee altitude
170.595 km
Semi-major axis
6,548.739 km
Eccentricity
0
Inclination
30.9669°
RAAN
318.9857°
Arg. of periapsis
200.7346°
True anomaly
Unknown
Mean anomaly
247.261°
Eccentric anomaly
Unknown
Mean motion
4.0955 °/min
Orbital period
87.9 mins
BSTAR
0.0028079
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
|