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: 13 hours ago

TLE from 13 hours ago
0 H-2A R/B
1 43682U 18084L   26137.54947318  .00012366  00000-0  27140-3 0  9999
2 43682  98.8618   9.7735 0024609 141.5621 218.7382 15.43934159416395
Epoch: 2026-05-17T13:11Z
TLE epoch observation values (Epoch: 2026-05-17T13:11:14.482Z)
Latitude
Longitude
-63.28733°
Altitude
450.684 km
Speed
7.635 km/s
True Right ascension
00h 39m 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
11:14:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
448.272 km
Perigee altitude
414.757 km
Semi-major axis
6,809.652 km
Eccentricity
0.00246
Inclination
98.8618°
RAAN
9.7735°
Arg. of periapsis
141.5621°
True anomaly
218.56216°
Mean anomaly
218.7382°
Eccentric anomaly
218.65014°
Mean motion
3.86239 °/min
Orbital period
93.21 mins
BSTAR
0.0002714
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