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, 0.9 m
Radar Cross Section
2.585 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ETIHAD-SAT
1 63226U 25052S 26118.19145224 .00004600 00000-0 20623-3 0 9995
2 63226 97.4022 11.5519 0004199 337.0598 23.0450 15.21707743 62239Epoch: 2026-04-28T04:35Z
TLE epoch observation values (Epoch: 2026-04-28T04:35:41.473Z)
Latitude
-0.00002°
Longitude
86.45879°
Altitude
501.124 km
Speed
7.615 km/s
True Right ascension
00h 46m 12s
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
20:54:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
500.54 km
Perigee altitude
494.766 km
Semi-major axis
6,875.79 km
Eccentricity
0.00042
Inclination
97.4022°
RAAN
11.5519°
Arg. of periapsis
337.0598°
True anomaly
23.06384°
Mean anomaly
23.045°
Eccentric anomaly
23.05442°
Mean motion
3.80679 °/min
Orbital period
94.57 mins
BSTAR
0.00020623
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-04-28 17:21:52.237Z | 209.436° SW | 2026-04-28 17:23:52.237Z | 275.718° WNW | 31.174° | 2026-04-28 17:26:52.237Z | 331.023° NNW |
| 5 mins | 2026-04-29 06:24:52.237Z | 335.256° NNW | 2026-04-29 06:26:52.237Z | 290.027° WNW | 24.003° | 2026-04-29 06:29:52.237Z | 232.212° WSW |
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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