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 (7 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: 7 hours ago

TLE from 7 hours ago
0 H-2A R/B
1 43682U 18084L   26100.52868359  .00018045  00000-0  41078-3 0  9990
2 43682  98.8685 324.7501 0023077 272.3722  87.4879 15.42773565410682
Epoch: 2026-04-10T12:41Z
TLE epoch observation values (Epoch: 2026-04-10T12:41:18.262Z)
Latitude
0.00002°
Longitude
-64.33704°
Altitude
440.349 km
Speed
7.648 km/s
True Right ascension
21h 39m 00s
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
02:23:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
450.655 km
Perigee altitude
419.21 km
Semi-major axis
6,813.07 km
Eccentricity
0.00231
Inclination
98.8685°
RAAN
324.7501°
Arg. of periapsis
272.3722°
True anomaly
87.75212°
Mean anomaly
87.4879°
Eccentric anomaly
87.62001°
Mean motion
3.85948 °/min
Orbital period
93.28 mins
BSTAR
0.00041078
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