H-2A R/B, 38341

Orbit data source: Space-Track

H-2A R/B, 38341 is space debris in SSO originally from a launch on Thu, 17 May 2012 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
38341, 2012-025E
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)
2012-05-17 (14 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: 4 hours ago

TLE from 4 hours ago
0 H-2A R/B
1 38341U 12025E   26170.16384819  .00001875  00000-0  17147-3 0  9999
2 38341  98.4834 145.4724 0043512 342.7595  17.2143 14.95729074763387
Epoch: 2026-06-19T03:55Z
TLE epoch observation values (Epoch: 2026-06-19T03:55:56.483Z)
Latitude
-0.00007°
Longitude
179.0903°
Altitude
554.22 km
Speed
7.6 km/s
True Right ascension
09h 41m 53s
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
18:54:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
607.422 km
Perigee altitude
546.894 km
Semi-major axis
6,955.295 km
Eccentricity
0.00435
Inclination
98.4834°
RAAN
145.4724°
Arg. of periapsis
342.7595°
True anomaly
17.36263°
Mean anomaly
17.2143°
Eccentric anomaly
17.28839°
Mean motion
3.74171 °/min
Orbital period
96.21 mins
BSTAR
0.00017147
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