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 (11 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: 1 day ago

TLE from 1 day ago
0 GAOFEN 9 DEB
1 44600U 15047B   26257.59878147  .00001933  00000-0  34479-3 0  9998
2 44600  98.1396 183.9834 0150797 149.7512 211.2502 14.60982693578894
Epoch: 2026-09-14T14:22Z
TLE epoch observation values (Epoch: 2026-09-14T14:22:14.719Z)
Latitude
0.00001°
Longitude
-25.1547°
Altitude
784.557 km
Speed
7.413 km/s
True Right ascension
12h 15m 56s
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
06:30:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
793.62 km
Perigee altitude
580.538 km
Semi-major axis
7,065.216 km
Eccentricity
0.01508
Inclination
98.1396°
RAAN
183.9834°
Arg. of periapsis
149.7512°
True anomaly
210.36801°
Mean anomaly
211.2502°
Eccentric anomaly
210.80769°
Mean motion
3.65473 °/min
Orbital period
98.5 mins
BSTAR
0.00034479
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Other satellites on launch #47 in the year 2015 (2015-09-14 UTC)

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