ZHUHAI-1 OHS-04, 43443 (Decayed)

Orbit data source: Space-Track

ZHUHAI-1 OHS-04, 43443 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-04 details

Identifier	43443, 2018-040E
Orbit	Decayed
Last TLE update	2 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 2 months ago

0 ZHUHAI-1 OHS-04
1 43443U 18040E   24306.12134492  .10508589  23711-5  89737-3 0  9994
2 43443  97.0829 356.5677 0008520 256.5334 103.5016 16.39479399363027

Epoch: 2024-11-01T02:54Z

Definitive object data (Epoch: 2024-11-01T02:54:44.201Z)

Latitude	-0.00008°
Longitude	-88.01114°
Altitude	171.754 km
Speed	7.802 km/s
True Right ascension	23h 46m 16s
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	169.556 km
Perigee altitude	158.408 km
Semi-major axis	6,542.119 km
Eccentricity	0.000852
Inclination	97.0829°
RAAN	356.5677°
Arg. of periapsis	256.5334°
True anomaly	103.59651°
Mean anomaly	103.5016°
Eccentric anomaly	103.54906°
Mean motion	4.10172 °/min
BSTAR	0.00089737
Orbital period	87.77 mins