JIADING 1, 43713 (Decayed)

Orbit data source: Space-Track

JIADING 1, 43713 was a payload satellite owned by SPACEOK (CN) in LEO that was launched on Mon, 19 Nov 2018 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

JIADING 1 details

Identifier	43713, 2018-094D
Orbit	Decayed
Last TLE update	3 months ago
Origin	SPACEOK (CN / PRC)
Manufacturer	SPACEOK
Mission	Decayed Commercial Communications
Bus & Motor	OKSAT, Unknown motor
Mass	50 kg wet, 50 kg dry
Launch date (UTC)	2018-11-19 (6 years ago)
Launch vehicle	CHANG ZHENG 2D
Launch site	Jiuquan Satellite Launch Center, China (JSC)
Object type	Payload Rocket body Debris
Shape & HBR	Box + 2 Pan, 2 m
Radar Cross Section	0.683 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 3 months ago

0 JIADING 1
1 43713U 18094D   24276.96673845  .17782445  26199-5  22415-3 0  9996
2 43713  97.3123 306.1131 0009377 242.3401 117.6952 16.49318177328025

Epoch: 2024-10-02T23:12Z

Definitive object data (Epoch: 2024-10-02T23:12:06.202Z)

Latitude	-0.00003°
Longitude	-54.07126°
Altitude	147.244 km
Speed	7.816 km/s
True Right ascension	20h 24m 27s
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	144.033 km
Perigee altitude	131.813 km
Semi-major axis	6,516.06 km
Eccentricity	0.0009377
Inclination	97.3123°
RAAN	306.1131°
Arg. of periapsis	242.3401°
True anomaly	117.79029°
Mean anomaly	117.6952°
Eccentric anomaly	117.74275°
Mean motion	4.12635 °/min
BSTAR	0.00022415
Orbital period	87.24 mins