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PAKSAT 1 (ANATOLIA 1), 23779

Orbit data source: Space-Track

PAKSAT 1 (ANATOLIA 1), 23779 is a Pakistani payload satellite in GEO that was launched on Thu, 01 Feb 1996 UTC via an ATLAS IIAS 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
23779, 1996-006A
Orbit
GEO
Last TLE update
20 hours ago
Origin
Manufacturer
Hughes
Mission
Non-operational Commercial Communications
Bus & Motor
HS-601, R-4D-11-300
Mass
2,989 kg wet, ~1,600 kg dry
Launch date (UTC)
1996-02-01 (30 years ago)
Launch vehicle
ATLAS IIAS
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Hex Poly + 2 Pan, 10.0 m
Radar Cross Section
25.555 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 20 hours ago
0 PAKSAT 1 (ANATOLIA 1)
1 23779U 96006A   25218.41572505 -.00000205  00000-0  00000-0 0  9994
2 23779  10.2038  48.6335 0007686 153.8645  66.7995  0.99599178107717
Epoch: 2025-08-06T09:58Z
TLE epoch observation values (Epoch: 2025-08-06T09:58:38.644Z)
Latitude
-6.64156°
Longitude
164.06898°
Altitude
35,964.216 km
Speed
3.069 km/s
True Right ascension
17h 55m 41s
True Declination
-6° 38' 06"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
2.39886°
Longitude
110.43907°
Altitude
35,943.841 km
Speed
3.07 km/s
Apparent Right ascension
13h 54m 53s
Apparent Declination
-3° 04' 50"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
20:30:17
Azimuth
273.329° WNW
Elevation
-8.763°
Doppler factor
1
Orbital elements
Apogee altitude
36,009.783 km
Perigee altitude
35,944.674 km
Semi-major axis
42,355.365 km
Eccentricity
0.00077
Inclination
10.2038°
RAAN
48.6335°
Arg. of periapsis
153.8645°
True anomaly
66.88048°
Mean anomaly
66.7995°
Eccentric anomaly
66.83999°
Mean motion
0.24899 °/min
Orbital period
1,445.85 mins
BSTAR
0
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Other satellites on launch #6 in the year 1996 (1996-02-01 UTC)
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