DECAYED

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.

Not visible in the next 10 days
H-2A R/B details
Identifier
45166, 2020-009B
Orbit
Decayed
Last TLE update8 months ago
Origin
Flag of JPMHI (JP / JPN)
ManufacturerMHI Tobishima
MissionDecayed spacecraft
Bus & MotorH-2A STAGE 2, Unknown motor
Mass4,000 kg wet, 4,000 kg dry
Launch date (UTC)
2020-02-09 (5 years ago)
Launch vehicleUnknown
Launch site
Tanegashima Space Center (TNSTA)
Object type
Payload
Rocket body
Debris
Shape & HBRCyl, 9.2 m
Radar Cross Section35.186 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)
Latitude80.2214°
Longitude-53.0038°
Altitude136.426 km
Speed7.828 km/s
True Right ascension07h 21m 21s
True Declination80° 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 altitude120.644 km
Perigee altitude108.19 km
Semi-major axis6,492.554 km
Eccentricity0.0009591
Inclination96.9487°
RAAN155.0121°
Arg. of periapsis232.7556°
True anomaly210.27695°
Mean anomaly210.3324°
Eccentric anomaly210.30467°
Mean motion4.14877 °/min
BSTAR0.00020022
Orbital period86.77 mins
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Other satellites on launch #9 in the year 2020 (2020-02-09 UTC)

H-2A R/B Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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