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.
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41341 intel report (Beta)
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Identifier
Orbit
Country
JP / JPNRelated 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)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl, 5.0 m
Radar Cross Section
35.186 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 H-2A R/B
1 41341U 16012E 26262.45131323 .00053883 00000-0 50025-3 0 9995
2 41341 30.6208 330.4645 0004304 194.2739 165.7786 15.66087059586281Epoch: 2026-09-19T10:49Z
TLE epoch observation values (Epoch: 2026-09-19T10:49:53.463Z)
Latitude
-0.00002°
Longitude
169.63205°
Altitude
371.364 km
Speed
7.688 km/s
True Right ascension
22h 01m 51s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:46:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
377.013 km
Perigee altitude
371.2 km
Semi-major axis
6,752.244 km
Eccentricity
0.00043
Inclination
30.6208°
RAAN
330.4645°
Arg. of periapsis
194.2739°
True anomaly
165.79071°
Mean anomaly
165.7786°
Eccentric anomaly
165.78466°
Mean motion
3.91175 °/min
Orbital period
92.03 mins
BSTAR
0.00050025
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Other satellites on launch #12 in the year 2016 (2016-02-17 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.H-2A R/B Visibility
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
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| H-2A R/B is likely not visible in the next few days. |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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