DECAYED
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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 update4 months ago
Origin
Flag of CNGuodian Gaokeji (CN / PRC)
ManufacturerShanghai ASES
MissionDecayed Commercial Communications
Bus & MotorSTARLIGHTB, Unknown motor
Mass40 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 & HBRBox, Unknown HBR
Radar Cross Section0.195 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 4 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°
Altitude136.516 km
Speed7.824 km/s
True Right ascension18h 58m 55s
True Declination0° 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 altitude137.463 km
Perigee altitude120.924 km
Semi-major axis6,507.33 km
Eccentricity0.0012708
Inclination97.0805°
RAAN284.732°
Arg. of periapsis264.3592°
True anomaly95.7715°
Mean anomaly95.6266°
Eccentric anomaly95.69905°
Mean motion4.13465 °/min
BSTAR0.00012274
Orbital period87.07 mins
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TIANQI-5 Visibility forecast

Observer location: undefined°, undefined

This satellite is decayed
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