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XW-2B, 40911

Orbit data source: Space-Track

XW-2B, 40911 is 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-2B details

Identifier	40911, 2015-049N
Orbit	LEO
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-2B
1 40911U 15049N   24327.12054824  .12327907  26494-5  35331-3 0  9997
2 40911  97.4275 356.1968 0008296 243.8788 116.1661 16.44814145509299

Epoch: 2024-11-22T02:53Z

Definitive object data (Epoch: 2024-11-22T02:53:35.367Z)

Latitude	-0.00003°
Longitude	-108.79305°
Altitude	158.678 km
Speed	7.809 km/s
True Right ascension	23h 44m 47s
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	155.246 km
Perigee altitude	144.414 km
Semi-major axis	6,527.967 km
Eccentricity	0.0008296
Inclination	97.4275°
RAAN	356.1968°
Arg. of periapsis	243.8788°
True anomaly	116.25138°
Mean anomaly	116.1661°
Eccentric anomaly	116.20875°
Mean motion	4.11506 °/min
BSTAR	0.00035331
Orbital period	87.48 mins