CZ-2D DEB, 44606

Orbit data source: Space-Track

CZ-2D DEB, 44606 is space debris in SSO originally from a launch on Fri, 11 Nov 2016 UTC launched from the Jiuquan Satellite Launch Center, China (JSC). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
44606, 2016-068F
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2016-11-11 (9 years ago)
Launch vehicle
Unknown
Launch site
Jiuquan Satellite Launch Center, China (JSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 CZ-2D DEB
1 44606U 16068F   26075.00388127  .00000492  00000-0  33128-3 0  9995
2 44606  98.4310 160.1752 0224866 105.1219 257.4937 13.92887662473469
Epoch: 2026-03-16T00:05Z
TLE epoch observation values (Epoch: 2026-03-16T00:05:35.341Z)
Latitude
-0°
Longitude
-14.82464°
Altitude
960.446 km
Speed
7.352 km/s
True Right ascension
10h 40m 42s
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
00:51:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,079.722 km
Perigee altitude
751.695 km
Semi-major axis
7,293.846 km
Eccentricity
0.02249
Inclination
98.431°
RAAN
160.1752°
Arg. of periapsis
105.1219°
True anomaly
254.99408°
Mean anomaly
257.4937°
Eccentric anomaly
256.24228°
Mean motion
3.48424 °/min
Orbital period
103.32 mins
BSTAR
0.00033128
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