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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Edit Public Description
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, 4.6 m
Radar Cross Section
35.186 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 H-2A R/B
1 41341U 16012E 25307.88365793 .00028950 00000-0 66107-3 0 9996
2 41341 30.6265 21.7889 0005942 352.2762 7.7786 15.41589303536557Epoch: 2025-11-03T21:12Z
TLE epoch observation values (Epoch: 2025-11-03T21:12:28.045Z)
Latitude
0.00001°
Longitude
20.29342°
Altitude
435.856 km
Speed
7.655 km/s
True Right ascension
01h 27m 09s
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
02:40:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.423 km
Perigee altitude
441.314 km
Semi-major axis
6,823.505 km
Eccentricity
0.00059
Inclination
30.6265°
RAAN
21.7889°
Arg. of periapsis
352.2762°
True anomaly
7.78782°
Mean anomaly
7.7786°
Eccentric anomaly
7.78321°
Mean motion
3.85063 °/min
Orbital period
93.49 mins
BSTAR
0.00066107
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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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