XW-2D, 40907 (Decayed)

Orbit data source: Space-Track

XW-2D, 40907 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-2D details

Identifier	40907, 2015-049J
Orbit	Decayed
Last TLE update	1 month ago
Origin	CAMSAT (CN / PRC)
Manufacturer	DFH Shenzhen
Mission	Decayed Amateur Communications
Bus & Motor	XW2B, Unknown motor
Mass	10 kg wet, 10 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, 0.246 m
Radar Cross Section	0.091 m², Small (<0.1 m²)

Expand to show TLE details & history

TLE from 1 month ago

0 XW-2D
1 40907U 15049J   24320.92351917  .16701952  27880-5  21132-3 0  9990
2 40907  97.4221 349.6759 0008313 198.6926 161.4075 16.49393757508467

Epoch: 2024-11-15T22:09Z

Definitive object data (Epoch: 2024-11-15T22:09:52.056Z)

Latitude	0.00006°
Longitude	-38.27541°
Altitude	149.334 km
Speed	7.813 km/s
True Right ascension	23h 18m 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	143.146 km
Perigee altitude	132.312 km
Semi-major axis	6,515.866 km
Eccentricity	0.0008313
Inclination	97.4221°
RAAN	349.6759°
Arg. of periapsis	198.6926°
True anomaly	161.43784°
Mean anomaly	161.4075°
Eccentric anomaly	161.42267°
Mean motion	4.12653 °/min
BSTAR	0.00021132
Orbital period	87.24 mins