DECAYED

OBJECT A, 40899 (Decayed)

Orbit data source: Space-Track

You're viewing an Uncataloged Satellite

Recently launched and/or uncataloged satellites may have evolving metadata. Metadata may include but not limited to: Owner, Maufacturer, Bus, Motor, and Mission.

OBJECT A, 40899 was a Chinese satellite in LEO that was launched on Sat, 19 Sep 2015 UTC via a CHANG ZHENG 6 launch vehicle from the Taiyaun Space Center, China (TSC). Unknown objects in Earth's orbit typically refer to objects detected orbiting the Earth but have not yet been identified or cataloged. These objects could be anything from previously untracked satellites, spent rocket stages, debris from satellite collisions, or even natural meteoroids temporarily captured by Earth's gravity. This object's orbit decayed before it could be identified.

Not visible in the next 10 days
Identifier
40899, 2015-049A
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
None
Manufacturer
Unknown
Mission
Decayed Amateur Communications
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
2015-09-19 (10 years ago)
Launch vehicle
CHANG ZHENG 6
Launch site
Taiyaun Space Center, China (TSC)
Object type
Unknown
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.475 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 8 months ago

TLE from 8 months ago
0 OBJECT A
1 40899U 15049A   25089.22128863  .15801369  26525-5  17247-3 0  9997
2 40899  97.3955 125.4220 0009888 247.1923 112.8338 16.50187745529137
Epoch: 2025-03-30T05:18Z
TLE epoch observation values (Epoch: 2025-03-30T05:18:39.337Z)
Latitude
-0°
Longitude
-142.09655°
Altitude
144.613 km
Speed
7.818 km/s
True Right ascension
08h 21m 41s
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
01:57:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
142.076 km
Perigee altitude
129.195 km
Semi-major axis
6,513.772 km
Eccentricity
0.00099
Inclination
97.3955°
RAAN
125.422°
Arg. of periapsis
247.1923°
True anomaly
112.93818°
Mean anomaly
112.8338°
Eccentric anomaly
112.88599°
Mean motion
4.12852 °/min
Orbital period
87.2 mins
BSTAR
0.00017247
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