GAOFEN 9 DEB, 44600

Orbit data source: Space-Track

GAOFEN 9 DEB, 44600 is space debris in SSO originally from a launch on Mon, 14 Sep 2015 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
44600, 2015-047B
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2015-09-14 (10 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: 19 hours ago

TLE from 19 hours ago
0 GAOFEN 9 DEB
1 44600U 15047B   25291.73987096  .00006913  00000-0  12748-2 0  9992
2 44600  98.1267 219.2025 0159480 103.5069 258.3956 14.57858208530623
Epoch: 2025-10-18T17:45Z
TLE epoch observation values (Epoch: 2025-10-18T17:45:24.850Z)
Latitude
0.00002°
Longitude
-74.6176°
Altitude
727.515 km
Speed
7.479 km/s
True Right ascension
14h 36m 48s
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
08:06:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
810.015 km
Perigee altitude
584.341 km
Semi-major axis
7,075.315 km
Eccentricity
0.01595
Inclination
98.1267°
RAAN
219.2025°
Arg. of periapsis
103.5069°
True anomaly
256.61289°
Mean anomaly
258.3956°
Eccentric anomaly
257.50349°
Mean motion
3.64691 °/min
Orbital period
98.71 mins
BSTAR
0.0012748
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Other satellites on launch #47 in the year 2015 (2015-09-14 UTC)

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