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ASIASAT 4, 27718

Orbit data source: Space-Track

ASIASAT 4, 27718 is a payload satellite in GEO that was launched on Sat, 12 Apr 2003 UTC via an ATLAS 3B 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
27718, 2003-014A
Orbit
GEO
Last TLE update
9 hours ago
Origin
Manufacturer
Boeing/ES
Mission
Operational Commercial Communications
Bus & Motor
HS-601HP, R-4D-14-350
Mass
4,137 kg wet, ~2,000 kg dry
Launch date (UTC)
2003-04-12 (22 years ago)
Launch vehicle
ATLAS 3B
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 2 Pan, 26.2 m
Radar Cross Section
46.266 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 ASIASAT 4
1 27718U 03014A   25138.83486738 -.00000211  00000-0  00000-0 0  9994
2 27718   3.6959  80.7243 0002113 339.8906 264.2323  1.00270328 41345
Epoch: 2025-05-18T20:02Z
TLE epoch observation values (Epoch: 2025-05-18T20:02:12.541Z)
Latitude
-3.32304°
Longitude
147.46286°
Altitude
35,787.903 km
Speed
3.075 km/s
True Right ascension
21h 39m 05s
True Declination
-3° 19' 11"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
1.34094°
Longitude
-75.52005°
Altitude
35,779.632 km
Speed
3.075 km/s
Apparent Right ascension
06h 22m 40s
Apparent Declination
-4° 01' 26"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
13:56:39
Azimuth
282.413° WNW
Elevation
-20.49°
Doppler factor
1
Orbital elements
Apogee altitude
35,796.977 km
Perigee altitude
35,779.158 km
Semi-major axis
42,166.204 km
Eccentricity
0.00021
Inclination
3.6959°
RAAN
80.7243°
Arg. of periapsis
339.8906°
True anomaly
Unknown
Mean anomaly
264.2323°
Eccentric anomaly
Unknown
Mean motion
0.25067 °/min
Orbital period
1,436.17 mins
BSTAR
0
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27718 neighbors
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Other satellites on launch #14 in the year 2003 (2003-04-12 UTC)

ASIASAT 4 Visibility

Observer location: undefined°, undefined°

ASIASAT 4 is not visible in the next 10 days
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