DECAYED

H-2A R/B, 36105 (Decayed)

Orbit data source: Space-Track

H-2A R/B, 36105 was space debris in LEO originally from a launch on Sat, 28 Nov 2009 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	36105, 2009-066B
Orbit	Decayed
Last TLE update	1 month ago
Origin	MHI (JP / JPN)
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)	2009-11-28 (15 years ago)
Launch vehicle	Unknown
Launch site	Tanegashima Space Center (TNSTA)
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 1 month ago

0 H-2A R/B
1 36105U 09066B   24333.53816314  .11214308  26859-5  60091-3 0  9996
2 36105  97.3617 328.5331 0005691 209.7958 278.6503 16.42249630828754

Epoch: 2024-11-28T12:54Z

Definitive object data (Epoch: 2024-11-28T12:54:57.295Z)

Latitude	51.13619°
Longitude	-103.95151°
Altitude	167.607 km
Speed	7.811 km/s
True Right ascension	10h 30m 49s
True Declination	50° 57' 10"
Sunlit	Object was in full shadow 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	160.347 km
Perigee altitude	152.909 km
Semi-major axis	6,534.765 km
Eccentricity	0.0005691
Inclination	97.3617°
RAAN	328.5331°
Arg. of periapsis	209.7958°
True anomaly	278.58582°
Mean anomaly	278.6503°
Eccentric anomaly	278.61806°
Mean motion	4.10864 °/min
BSTAR	0.00060091
Orbital period	87.62 mins