H-2A R/B, 43067

Orbit data source: Space-Track

H-2A R/B, 43067 is space debris in SSO 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	SSO
Last TLE update	9 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 9 hours ago

0 H-2A R/B
1 43067U 17082C   24361.21407355  .00067249  00000-0  10704-2 0  9993
2 43067  98.3378 341.8099 0055414 111.7643 248.9516 15.51271596386976

Epoch: 2024-12-26T05:08Z

Definitive object data (Epoch: 2024-12-26T05:08:15.954Z)

Latitude	-0.00007°
Longitude	169.54675°
Altitude	429.817 km
Speed	7.646 km/s
True Right ascension	22h 47m 14s
True Declination	0° 00' 00"
Sunlit	Object was in daylight at TLE epoch

Visualization TLE readout

Latitude	-64.37758°
Longitude	-27.72067°
Altitude	463.948 km
Speed	7.618 km/s
Apparent Right ascension	03h 46m 26s
Apparent Declination	-68° 35' 09"
Sunlit	Object is in daylight

Visualization observer readout

Local Sidereal Time	13:17:29
Azimuth	202.725° SW
Elevation	-55.116°
Doppler factor	1

Orbital elements

Apogee altitude	447.595 km
Perigee altitude	372.364 km
Semi-major axis	6,788.116 km
Eccentricity	0.0055414
Inclination	98.3378°
RAAN	341.8099°
Arg. of periapsis	111.7643°
True anomaly	248.36045°
Mean anomaly	248.9516°
Eccentric anomaly	248.65588°
Mean motion	3.88078 °/min
BSTAR	0.0010704
Orbital period	92.76 mins