GAOFEN 3 DEB, 42680

Orbit data source: Space-Track

GAOFEN 3 DEB, 42680 is space debris in SSO originally from a launch on Tue, 09 Aug 2016 UTC launched from the Taiyaun Space Center, China (TSC). 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
42680, 2016-049E
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2016-08-09 (10 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.057 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 GAOFEN 3 DEB
1 42680U 16049E   26314.78370052  .00001720  00000-0  43315-3 0  9997
2 42680  98.4195 330.8977 0016106  23.9206 336.2734 14.52363795537627
Epoch: 2026-11-10T18:48Z
TLE epoch observation values (Epoch: 2026-11-10T18:48:31.724Z)
Latitude
-0.00007°
Longitude
-1.17541°
Altitude
710.444 km
Speed
7.506 km/s
True Right ascension
22h 03m 35s
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
10:20:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
726.464 km
Perigee altitude
703.616 km
Semi-major axis
7,093.177 km
Eccentricity
0.00161
Inclination
98.4195°
RAAN
330.8977°
Arg. of periapsis
23.9206°
True anomaly
336.199°
Mean anomaly
336.2734°
Eccentric anomaly
336.23621°
Mean motion
3.63314 °/min
Orbital period
99.09 mins
BSTAR
0.00043315
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Other satellites on launch #49 in the year 2016 (2016-08-09 UTC)

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