XW-2F, 40910 (Decayed)

Orbit data source: Space-Track

XW-2F, 40910 was a payload satellite owned by CAMSAT (CN) in LEO that was launched on Sat, 19 Sep 2015 UTC via a CHANG ZHENG 6 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

XW-2F details

Identifier	40910, 2015-049M
Orbit	Decayed
Last TLE update	9 months ago
Origin	CAMSAT (CN / PRC)
Manufacturer	DFH Shenzhen
Mission	Decayed Amateur Communications
Bus & Motor	XW2E, Unknown motor
Mass	1.5 kg wet, 1.5 kg dry
Launch date (UTC)	2015-09-19 (9 years ago)
Launch vehicle	CHANG ZHENG 6
Launch site	Taiyaun Space Center, China (TSC)
Object type	Payload Rocket body Debris
Shape & HBR	Box, 0.116 m
Radar Cross Section	0.020 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 9 months ago

0 XW-2F
1 40910U 15049M   24092.20923921  .16747303  26701-5  28112-3 0  9997
2 40910  97.4046 122.6776 0010391 231.3491 128.6883 16.47481859473951

Epoch: 2024-04-01T05:01Z

Definitive object data (Epoch: 2024-04-01T05:01:18.267Z)

Latitude	-0.00006°
Longitude	-142.70128°
Altitude	153.479 km
Speed	7.811 km/s
True Right ascension	08h 10m 42s
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	149.549 km
Perigee altitude	135.997 km
Semi-major axis	6,520.91 km
Eccentricity	0.0010391
Inclination	97.4046°
RAAN	122.6776°
Arg. of periapsis	231.3491°
True anomaly	128.78117°
Mean anomaly	128.6883°
Eccentric anomaly	128.73474°
Mean motion	4.12174 °/min
BSTAR	0.00028112
Orbital period	87.34 mins