Showing default

QIANFAN-57, 62787

Orbit data source: Space-Track

QIANFAN-57, 62787 is a Chinese payload satellite in LEO that was launched on Thu, 23 Jan 2025 UTC via a CHANG ZHENG 6A launch vehicle from the Taiyaun Space Center, China (TSC). Payload-class satellites include a variety of spacecraft 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.

Loading next visibility...
Identifier
62787, 2025-016C
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
Manufacturer
SECM
Mission
Operational Commercial Communications
Bus & Motor
QIANFAN, Unknown motor
Mass
267 kg wet, ~267 kg dry
Launch date (UTC)
2025-01-23 (2 years ago)
Launch vehicle
CHANG ZHENG 6A
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 1 Pan, 5.0 m
Radar Cross Section
13.200 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 QIANFAN-57
1 62787U 25016C   26305.77577323  .00000099  00000-0  13386-3 0  9993
2 62787  88.9734  69.5647 0001038  99.7845 260.3423 13.51032089 90957
Epoch: 2026-11-01T18:37Z
TLE epoch observation values (Epoch: 2026-11-01T18:37:06.807Z)
Latitude
-0.00004°
Longitude
109.22404°
Altitude
1,071.547 km
Speed
7.316 km/s
True Right ascension
04h 38m 15s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
22:56:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,066.287 km
Perigee altitude
1,064.742 km
Semi-major axis
7,443.652 km
Eccentricity
0.0001
Inclination
88.9734°
RAAN
69.5647°
Arg. of periapsis
99.7845°
True anomaly
260.33057°
Mean anomaly
260.3423°
Eccentric anomaly
260.33644°
Mean motion
3.37959 °/min
Orbital period
106.52 mins
BSTAR
0.00013386
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|