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: 21 hours ago

TLE from 21 hours ago
0 H-2A DEB
1 43068U 17082D   25259.99104733  .00080832  00000-0  13042-2 0  9991
2 43068  98.0040  50.8012 0069547 164.9347 195.3996 15.49848856421136
Epoch: 2025-09-16T23:47Z
TLE epoch observation values (Epoch: 2025-09-16T23:47:06.489Z)
Latitude
-0.00005°
Longitude
57.85076°
Altitude
465.877 km
Speed
7.608 km/s
True Right ascension
03h 23m 12s
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
13:57:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
461.359 km
Perigee altitude
366.883 km
Semi-major axis
6,792.258 km
Eccentricity
0.00695
Inclination
98.004°
RAAN
50.8012°
Arg. of periapsis
164.9347°
True anomaly
195.18973°
Mean anomaly
195.3996°
Eccentric anomaly
195.29449°
Mean motion
3.87723 °/min
Orbital period
92.85 mins
BSTAR
0.0013042
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Other satellites on launch #82 in the year 2017 (2017-12-23 UTC)

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