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ASIASAT 8, 40107

Orbit data source: Space-Track

ASIASAT 8, 40107 is a payload satellite owned by Asiasat (HK) in GEO that was launched on Tue, 05 Aug 2014 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

Not visible in the next 10 days
Identifier
40107, 2014-046A
Orbit
GEO
Last TLE update
11 hours ago
Origin
Manufacturer
SS/Loral (MDA)
Mission
Operational Commercial Communications
Bus & Motor
LS-1300LL, R-4D
Mass
4,535 kg wet, ~2,500 kg dry
Launch date (UTC)
Icon of a cake. It is the launch day of the satellite!2014-08-05 (11 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 13.5 m
Radar Cross Section
26.964 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 11 hours ago
0 ASIASAT 8
1 40107U 14046A   25216.89489414 -.00000324  00000-0  00000-0 0  9990
2 40107   0.0373 244.2050 0001557 240.6000 256.3522  1.00270124 98979
Epoch: 2025-08-04T21:28Z
TLE epoch observation values (Epoch: 2025-08-04T21:28:38.853Z)
Latitude
-0.01385°
Longitude
105.28672°
Altitude
35,788.111 km
Speed
3.075 km/s
True Right ascension
01h 24m 34s
True Declination
0° 00' 50"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
0.01367°
Longitude
-88.98691°
Altitude
35,783.519 km
Speed
3.075 km/s
Apparent Right ascension
12h 15m 14s
Apparent Declination
-4° 59' 46"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
22:25:44
Azimuth
317.557° NNW
Elevation
-47.256°
Doppler factor
1
Orbital elements
Apogee altitude
35,794.696 km
Perigee altitude
35,781.566 km
Semi-major axis
42,166.268 km
Eccentricity
0.00016
Inclination
0.0373°
RAAN
244.205°
Arg. of periapsis
240.6°
True anomaly
256.33486°
Mean anomaly
256.3522°
Eccentric anomaly
256.34353°
Mean motion
0.25067 °/min
Orbital period
1,436.17 mins
BSTAR
0
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Other satellites on launch #46 in the year 2014 (2014-08-05 UTC)
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