ARABSAT 2A, 23948
Orbit data source: Space-Track
ARABSAT 2A, 23948 is a payload satellite owned by Arabsat (SA) in GEO that was launched on Tue, 09 Jul 1996 UTC via an ARIANE 44L launch vehicle from the French Guiana (FRGUI). 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.
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23948 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ABRelated business
Manufacturer
Ae/Cannes
Mission
Non-operational Commercial Communications
Bus & Motor
SPACEBUS 3000, S400
Mass
2,617 kg wet, 1,108 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Hex Poly + 2 Pan, 13.2 m
Radar Cross Section
22.988 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ARABSAT 2A
1 23948U 96040A 25251.02315711 -.00000069 00000-0 00000-0 0 9996
2 23948 14.0791 11.0824 0006781 164.6883 198.1312 0.99229979106068Epoch: 2025-09-08T00:33Z
TLE epoch observation values (Epoch: 2025-09-08T00:33:20.774Z)
Latitude
0.66792°
Longitude
18.09892°
Altitude
36,108.173 km
Speed
3.062 km/s
True Right ascension
00h 55m 04s
True Declination
0° 40' 02"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
19:54:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
36,110.967 km
Perigee altitude
36,053.382 km
Semi-major axis
42,460.311 km
Eccentricity
0.00068
Inclination
14.0791°
RAAN
11.0824°
Arg. of periapsis
164.6883°
True anomaly
198.10704°
Mean anomaly
198.1312°
Eccentric anomaly
198.11912°
Mean motion
0.24807 °/min
Orbital period
1,451.22 mins
BSTAR
0
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Other satellites on launch #40 in the year 1996 (1996-07-09 UTC)
ARABSAT 2A Visibility
Observer location: undefined°, undefined°
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| ARABSAT 2A is likely not visible in the next few days |
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23948 neighbors
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Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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