H-2A R/B, 43067

Orbit data source: Space-Track

H-2A R/B, 43067 is space debris in LEO originally from a launch on Sat, 23 Dec 2017 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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H-2A R/B details

Identifier	43067, 2017-082C
Orbit	LEO
Last TLE update	22 hours ago
Origin	MHI (JP / JPN)
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)	2017-12-23 (7 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 22 hours ago

0 H-2A R/B
1 43067U 17082C   24347.46660158  .00046657  00000-0  79286-3 0  9997
2 43067  98.3376 325.9101 0054890 159.1523 201.1982 15.49587061384847

Epoch: 2024-12-12T11:11Z

Definitive object data (Epoch: 2024-12-12T11:11:54.376Z)

Latitude	0.00002°
Longitude	76.28701°
Altitude	455.849 km
Speed	7.619 km/s
True Right ascension	21h 43m 38s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	79.19438°
Longitude	27.56786°
Altitude	419.784 km
Speed	7.673 km/s
Apparent Right ascension	19h 29m 18s
Apparent Declination	22° 53' 33"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	07:44:56
Azimuth	4.043° NNE
Elevation	-27.086°
Doppler factor	1

Orbital elements

Apogee altitude	452.189 km
Perigee altitude	377.615 km
Semi-major axis	6,793.039 km
Eccentricity	0.005489
Inclination	98.3376°
RAAN	325.9101°
Arg. of periapsis	159.1523°
True anomaly	200.97221°
Mean anomaly	201.1982°
Eccentric anomaly	201.08506°
Mean motion	3.87656 °/min
BSTAR	0.00079286
Orbital period	92.87 mins