ZHEDA PIXING 3A, 45795 (Decayed)

Orbit data source: Space-Track

ZHEDA PIXING 3A, 45795 was a payload satellite owned by Zhejiang (CN) in LEO that was launched on Wed, 17 Jun 2020 UTC via a CHANG ZHENG 2D 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

ZHEDA PIXING 3A details

Identifier	45795, 2020-039B
Orbit	Decayed
Last TLE update	2 months ago
Origin	Zhejiang (CN / PRC)
Manufacturer	Zhejiang
Mission	Decayed Amateur Technology
Bus & Motor	Unknown
Mass	12 kg wet, 12 kg dry
Launch date (UTC)	2020-06-17 (5 years ago)
Launch vehicle	CHANG ZHENG 2D
Launch site	Jiuquan Satellite Launch Center, China (JSC)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 1 Truss, Unknown HBR
Radar Cross Section	0.094 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 2 months ago

0 ZHEDA PIXING 3A
1 45795U 20039B   24299.68164617  .14036921  26590-5  12355-3 0  9991
2 45795  97.4538  89.0895 0012144 259.3589 100.6349 16.51430924244154

Epoch: 2024-10-25T16:21Z

Definitive object data (Epoch: 2024-10-25T16:21:34.229Z)

Latitude	0.00002°
Longitude	169.14947°
Altitude	140.304 km
Speed	7.821 km/s
True Right ascension	05h 56m 21s
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	140.272 km
Perigee altitude	124.459 km
Semi-major axis	6,510.502 km
Eccentricity	0.0012144
Inclination	97.4538°
RAAN	89.0895°
Arg. of periapsis	259.3589°
True anomaly	100.77163°
Mean anomaly	100.6349°
Eccentric anomaly	100.70327°
Mean motion	4.13163 °/min
BSTAR	0.00012355
Orbital period	87.13 mins