ZHUHAI-1 OHS-03, 43442 (Decayed)

Orbit data source: Space-Track

ZHUHAI-1 OHS-03, 43442 was a payload satellite owned by Zhuhai Orbita (CN) in LEO that was launched on Thu, 26 Apr 2018 UTC via a CHANG ZHENG 11 launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days

ZHUHAI-1 OHS-03 details

Identifier	43442, 2018-040D
Orbit	Decayed
Last TLE update	3 months ago
Origin	Zhuhai Orbita (CN / PRC)
Manufacturer	Harbin
Mission	Decayed Commercial Imaging
Bus & Motor	OHS-1, Unknown motor
Mass	~69 kg wet, ~69 kg dry
Launch date (UTC)	2018-04-26 (7 years ago)
Launch vehicle	CHANG ZHENG 11
Launch site	Jiuquan Satellite Launch Center, China (JSC)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 1 m
Radar Cross Section	0.280 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 3 months ago

0 ZHUHAI-1 OHS-03
1 43442U 18040D   24276.19343411  .10148392  23560-5  51327-3 0  9997
2 43442  97.0784 327.8475 0014649 274.7255  85.2373 16.41238223358585

Epoch: 2024-10-02T04:38Z

Definitive object data (Epoch: 2024-10-02T04:38:32.707Z)

Latitude	0.00001°
Longitude	-113.18509°
Altitude	164.991 km
Speed	7.808 km/s
True Right ascension	21h 51m 23s
True Declination	0° 00' 00"
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	168.879 km
Perigee altitude	149.726 km
Semi-major axis	6,537.44 km
Eccentricity	0.0014649
Inclination	97.0784°
RAAN	327.8475°
Arg. of periapsis	274.7255°
True anomaly	85.40461°
Mean anomaly	85.2373°
Eccentric anomaly	85.32095°
Mean motion	4.10612 °/min
BSTAR	0.00051327
Orbital period	87.67 mins