ZHUHAI-1 OHS-01, 43439 (Decayed)

Orbit data source: Space-Track

ZHUHAI-1 OHS-01, 43439 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-01 details

Identifier	43439, 2018-040A
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	~50 kg wet, ~50 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-01
1 43439U 18040A   24315.57878628  .13816206  24199-5  25760-3 0  9992
2 43439  97.0750   4.3621 0009607 251.7763 108.2495 16.46965131364488

Epoch: 2024-11-10T13:53Z

Definitive object data (Epoch: 2024-11-10T13:53:27.134Z)

Latitude	-0.0001°
Longitude	105.78267°
Altitude	152.579 km
Speed	7.813 km/s
True Right ascension	00h 17m 26s
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	150.39 km
Perigee altitude	137.858 km
Semi-major axis	6,522.261 km
Eccentricity	0.0009607
Inclination	97.075°
RAAN	4.3621°
Arg. of periapsis	251.7763°
True anomaly	108.35401°
Mean anomaly	108.2495°
Eccentric anomaly	108.30176°
Mean motion	4.12046 °/min
BSTAR	0.0002576
Orbital period	87.37 mins