ETIHAD-SAT, 63226
Orbit data source: Space-Track
ETIHAD-SAT, 63226 is a payload satellite owned by Rashid Space Ctr (AE) in SSO that was launched on Sat, 15 Mar 2025 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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63226 intel report (Beta)
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Identifier
Orbit
Country
AE / UAERelated business
Manufacturer
MBRSC/SATREC
Mission
Operational Civil Radar Imaging
Bus & Motor
ETIHAD, Unknown motor
Mass
220 kg wet, ~200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 2.5 m
Radar Cross Section
2.585 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ETIHAD-SAT
1 63226U 25052S 26259.45711663 .00003600 00000-0 15753-3 0 9993
2 63226 97.3815 150.4557 0005339 162.6579 197.4841 15.22680811 83725Epoch: 2026-09-16T10:58Z
TLE epoch observation values (Epoch: 2026-09-16T10:58:14.876Z)
Latitude
-0.00004°
Longitude
-9.51471°
Altitude
504.355 km
Speed
7.61 km/s
True Right ascension
10h 01m 49s
True Declination
0° 00' 00"
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
03:53:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.389 km
Perigee altitude
491.05 km
Semi-major axis
6,872.857 km
Eccentricity
0.00053
Inclination
97.3815°
RAAN
150.4557°
Arg. of periapsis
162.6579°
True anomaly
197.46573°
Mean anomaly
197.4841°
Eccentric anomaly
197.47491°
Mean motion
3.80923 °/min
Orbital period
94.51 mins
BSTAR
0.00015753
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Other satellites on launch #52 in the year 2025 (2025-03-15 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.ETIHAD-SAT Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-17 17:03:44.323Z | 179.016° S | 2026-09-17 17:06:44.323Z | 266.872° W | 63.653° | 2026-09-17 17:09:44.323Z | 340.057° N |
| 5 mins | 2026-09-18 06:07:44.323Z | 344.637° N | 2026-09-18 06:09:44.323Z | 282.987° WNW | 41.053° | 2026-09-18 06:12:44.323Z | 217.613° SW |
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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