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.

Not visible in the next 10 days
Identifier
43068, 2017-082D
Orbit
SSO
Last TLE update
14 hours ago
Origin
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

TLE from 14 hours ago
0 H-2A DEB
1 43068U 17082D   25199.39716015  .00034436  00000-0  69655-3 0  9991
2 43068  97.9988 343.9987 0080926  20.9899 339.4637 15.42825280411770
Epoch: 2025-07-18T09:31Z
TLE epoch observation values (Epoch: 2025-07-18T09:31:54.636Z)
Latitude
-0.00001°
Longitude
-95.42816°
Altitude
389.27 km
Speed
7.706 km/s
True Right ascension
22h 55m 59s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
10.55579°
Longitude
-96.27763°
Altitude
385.418 km
Speed
7.71 km/s
Apparent Right ascension
23h 30m 45s
Apparent Declination
-14° 04' 07"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
12:22:47
Azimuth
27.461° NE
Elevation
-61.748°
Doppler factor
1
Orbital elements
Apogee altitude
489.871 km
Perigee altitude
379.603 km
Semi-major axis
6,812.874 km
Eccentricity
0.00809
Inclination
97.9988°
RAAN
343.9987°
Arg. of periapsis
20.9899°
True anomaly
339.13528°
Mean anomaly
339.4637°
Eccentric anomaly
339.2998°
Mean motion
3.85965 °/min
Orbital period
93.27 mins
BSTAR
0.00069655
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