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
Last TLE update
17 hours ago
Origin
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
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history

TLE from 17 hours ago
0 GAOFEN 9 DEB
1 44600U 15047B   25199.26065963  .00004154  00000-0  78304-3 0  9993
2 44600  98.1225 128.9026 0161526  32.1895 328.9041 14.56960210517150
Epoch: 2025-07-18T06:15Z
TLE epoch observation values (Epoch: 2025-07-18T06:15:20.992Z)
Latitude
0.00001°
Longitude
98.75047°
Altitude
608.53 km
Speed
7.607 km/s
True Right ascension
08h 35m 36s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
24.39563°
Longitude
-76.85979°
Altitude
771.032 km
Speed
7.436 km/s
Apparent Right ascension
22h 18m 21s
Apparent Declination
-6° 14' 53"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
12:13:51
Azimuth
45.301° ENE
Elevation
-47.515°
Doppler factor
1
Orbital elements
Apogee altitude
814.419 km
Perigee altitude
585.755 km
Semi-major axis
7,078.224 km
Eccentricity
0.01615
Inclination
98.1225°
RAAN
128.9026°
Arg. of periapsis
32.1895°
True anomaly
327.93138°
Mean anomaly
328.9041°
Eccentric anomaly
328.41943°
Mean motion
3.64466 °/min
Orbital period
98.77 mins
BSTAR
0.00078304
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