Showing default

QIANFAN-134, 69079

Orbit data source: Space-Track

QIANFAN-134, 69079 is a Chinese payload satellite in LEO that was launched on Tue, 12 May 2026 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
69079, 2026-104G
Orbit
LEO
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Unknown
Mission
Operational spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2026-05-12 (1 week ago)
Launch vehicle
CHANG ZHENG 6A
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

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

TLE from 9 hours ago
0 QIANFAN-134
1 69079U 26104G   26140.61746336 -.02114383  00000-0 -11084+1 0  9991
2 69079  88.9859 344.7746 0008374 181.6118 178.5046 14.18560758  1178
Epoch: 2026-05-20T14:49Z
TLE epoch observation values (Epoch: 2026-05-20T14:49:08.834Z)
Latitude
0.00001°
Longitude
-115.78665°
Altitude
839.311 km
Speed
7.43 km/s
True Right ascension
22h 59m 05s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
08:18:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
833.211 km
Perigee altitude
821.144 km
Semi-major axis
7,205.315 km
Eccentricity
0.00084
Inclination
88.9859°
RAAN
344.7746°
Arg. of periapsis
181.6118°
True anomaly
178.5071°
Mean anomaly
178.5046°
Eccentric anomaly
178.50585°
Mean motion
3.54865 °/min
Orbital period
101.45 mins
BSTAR
-1.1084
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
|