H-2A DEB, 43068

Orbit data source: Space-Track

H-2A DEB, 43068 is space debris in SSO originally from a launch on Sat, 23 Dec 2017 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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Identifier
43068, 2017-082D
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
MELCO
Mission
Spacecraft
Bus & Motor
Unknown
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
2017-12-23 (8 years ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trunc Cone, 0.5 m
Radar Cross Section
0.533 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 H-2A DEB
1 43068U 17082D   25260.95946622  .00083686  00000-0  13432-2 0  9993
2 43068  98.0042  51.8760 0069166 161.4790 198.9002 15.50012584421286
Epoch: 2025-09-17T23:01Z
TLE epoch observation values (Epoch: 2025-09-17T23:01:37.881Z)
Latitude
0.00004°
Longitude
69.34022°
Altitude
464.31 km
Speed
7.609 km/s
True Right ascension
03h 27m 30s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:10:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
460.618 km
Perigee altitude
366.666 km
Semi-major axis
6,791.779 km
Eccentricity
0.00692
Inclination
98.0042°
RAAN
51.876°
Arg. of periapsis
161.479°
True anomaly
198.64555°
Mean anomaly
198.9002°
Eccentric anomaly
198.77267°
Mean motion
3.87764 °/min
Orbital period
92.84 mins
BSTAR
0.0013432
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Other satellites on launch #82 in the year 2017 (2017-12-23 UTC)

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