ARABSAT 5C, 37810
Orbit data source: Space-Track
ARABSAT 5C, 37810 is a payload satellite owned by Arabsat (SA) in GEO that was launched on Wed, 21 Sep 2011 UTC via an ARIANE 5ECA 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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37810 intel report (Beta)
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Identifier
Orbit
Country
ABRelated business
Manufacturer
Astrium/Toulouse
Mission
Operational Commercial Communications
Bus & Motor
EUROSTAR 3000, R-4D-15
Mass
4,619 kg wet, ~2,000 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan + 1 Dish, 15.4 m
Radar Cross Section
26.994 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 ARABSAT 5C
1 37810U 11049B 26183.23010193 .00000134 00000-0 00000-0 0 9991
2 37810 0.0523 22.0101 0003398 96.8331 264.2456 1.00271895 54180Epoch: 2026-07-02T05:31Z
TLE epoch observation values (Epoch: 2026-07-02T05:31:20.806Z)
Latitude
0.00123°
Longitude
19.94221°
Altitude
35,787.458 km
Speed
3.075 km/s
True Right ascension
01h 32m 13s
True Declination
0° 00' 04"
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
01:10:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,801.962 km
Perigee altitude
35,773.307 km
Semi-major axis
42,165.772 km
Eccentricity
0.00034
Inclination
0.0523°
RAAN
22.0101°
Arg. of periapsis
96.8331°
True anomaly
264.20686°
Mean anomaly
264.2456°
Eccentric anomaly
264.22623°
Mean motion
0.25067 °/min
Orbital period
1,436.15 mins
BSTAR
0
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Other satellites on launch #49 in the year 2011 (2011-09-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ARABSAT 5C Visibility
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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. |
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| ARABSAT 5C is likely not visible in the next few days. |
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37810 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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