TIANQI-5, 45019 (Decayed)

Orbit data source: Space-Track

TIANQI-5, 45019 was a payload satellite owned by Guodian Gaokeji (CN) in LEO that was launched on Wed, 15 Jan 2020 UTC via a CHANG ZHENG 2D launch vehicle from the Taiyaun Space Center, China (TSC). 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

TIANQI-5 details

Identifier	45019, 2020-003D
Orbit	Decayed
Last TLE update	5 months ago
Origin	Guodian Gaokeji (CN / PRC)
Manufacturer	Shanghai ASES
Mission	Decayed Commercial Communications
Bus & Motor	STARLIGHTB, Unknown motor
Mass	40 kg wet, ~40 kg dry
Launch date (UTC)	2020-01-15 (5 years ago)
Launch vehicle	CHANG ZHENG 2D
Launch site	Taiyaun Space Center, China (TSC)
Object type	Payload Rocket body Debris
Shape & HBR	Box, Unknown HBR
Radar Cross Section	0.195 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 5 months ago

0 TIANQI-5
1 45019U 20003D   24221.24340497  .16605158  24230-5  12274-3 0  9995
2 45019  97.0805 284.7320 0012708 264.3592  95.6266 16.52631078256214

Epoch: 2024-08-08T05:50Z

Definitive object data (Epoch: 2024-08-08T05:50:30.189Z)

Latitude	-0.00001°
Longitude	-120.12875°
Altitude	136.516 km
Speed	7.824 km/s
True Right ascension	18h 58m 55s
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	137.463 km
Perigee altitude	120.924 km
Semi-major axis	6,507.33 km
Eccentricity	0.0012708
Inclination	97.0805°
RAAN	284.732°
Arg. of periapsis	264.3592°
True anomaly	95.7715°
Mean anomaly	95.6266°
Eccentric anomaly	95.69905°
Mean motion	4.13465 °/min
BSTAR	0.00012274
Orbital period	87.07 mins