H-2A R/B, 45166 (Decayed)
Orbit data source: Space-Track
H-2A R/B, 45166 was space debris in LEO originally from a launch on Sun, 09 Feb 2020 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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45166 intel report (Beta)
H-2A R/B details
Identifier | |
Orbit | Decayed |
Last TLE update | 8 months ago |
Origin | |
Manufacturer | MHI Tobishima |
Mission | Decayed 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 | Payload Rocket body Debris |
Shape & HBR | Cyl, 9.2 m |
Radar Cross Section | 35.186 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 8 months ago
0 H-2A R/B
1 45166U 20009B 24113.86650667 .53867009 26681-5 20022-3 0 9993
2 45166 96.9487 155.0121 0009591 232.7556 210.3324 16.58268437235483
Epoch: 2024-04-22T20:47Z
Definitive object data (Epoch: 2024-04-22T20:47:46.176Z)
Latitude | 80.2214° |
Longitude | -53.0038° |
Altitude | 136.426 km |
Speed | 7.828 km/s |
True Right ascension | 07h 21m 21s |
True Declination | 80° 09' 29" |
Sunlit | Object was in daylight at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 120.644 km |
Perigee altitude | 108.19 km |
Semi-major axis | 6,492.554 km |
Eccentricity | 0.0009591 |
Inclination | 96.9487° |
RAAN | 155.0121° |
Arg. of periapsis | 232.7556° |
True anomaly | 210.27695° |
Mean anomaly | 210.3324° |
Eccentric anomaly | 210.30467° |
Mean motion | 4.14877 °/min |
BSTAR | 0.00020022 |
Orbital period | 86.77 mins |
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Other satellites on launch #9 in the year 2020 (2020-02-09 UTC)
IGS O-7, 45165 |
H-2A R/B, 45166 (Decayed) |
H-2A R/B Visibility forecast
Observer location: undefined°, undefined
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