H-2A R/B, 41341

Orbit data source: Space-Track

H-2A R/B, 41341 is space debris in LEO originally from a launch on Wed, 17 Feb 2016 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.

Not visible in the next 10 days
Identifier
41341, 2016-012E
Orbit
LEO
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)
2016-02-17 (10 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 41341U 16012E   26064.91115752  .00038549  00000-0  65352-3 0  9995
2 41341  30.6230 266.6722 0004293 223.7073 136.3229 15.50221954555456
Epoch: 2026-03-05T21:52Z
TLE epoch observation values (Epoch: 2026-03-05T21:52:04.009Z)
Latitude
-0.00005°
Longitude
135.00069°
Altitude
416.633 km
Speed
7.663 km/s
True Right ascension
17h 46m 41s
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
09:01:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
422.961 km
Perigee altitude
417.124 km
Semi-major axis
6,798.18 km
Eccentricity
0.00043
Inclination
30.623°
RAAN
266.6722°
Arg. of periapsis
223.7073°
True anomaly
136.35686°
Mean anomaly
136.3229°
Eccentric anomaly
136.33988°
Mean motion
3.87217 °/min
Orbital period
92.97 mins
BSTAR
0.00065352
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