H-2A R/B, 43682

Orbit data source: Space-Track

H-2A R/B, 43682 is space debris in SSO originally from a launch on Mon, 29 Oct 2018 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
43682, 2018-084L
Orbit
SSO
Country
Flag of JPJP / JPN
Related business
Manufacturer
MHI Tobishima
Mission
Spacecraft
Bus & Motor
H-2A STAGE 2, Unknown motor
Mass
4,000 kg wet, 4,000 kg dry
Launch date (UTC)
2018-10-29 (8 years ago)
Launch vehicle
Unknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 4.6 m
Radar Cross Section
35.186 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 H-2A R/B
1 43682U 18084L   26183.73226246  .00021852  00000-0  44927-3 0  9993
2 43682  98.8551  66.0241 0021750 346.2519  13.8130 15.45765966423521
Epoch: 2026-07-02T17:34Z
TLE epoch observation values (Epoch: 2026-07-02T17:34:27.476Z)
Latitude
-0.00007°
Longitude
-118.3608°
Altitude
417.829 km
Speed
7.668 km/s
True Right ascension
04h 24m 05s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
23:34:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
440.928 km
Perigee altitude
411.329 km
Semi-major axis
6,804.266 km
Eccentricity
0.00218
Inclination
98.8551°
RAAN
66.0241°
Arg. of periapsis
346.2519°
True anomaly
13.87266°
Mean anomaly
13.813°
Eccentric anomaly
13.84282°
Mean motion
3.86697 °/min
Orbital period
93.1 mins
BSTAR
0.00044927
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