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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Edit Public Description
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: 12 hours ago
TLE from 12 hours ago
0 ETIHAD-SAT
1 63226U 25052S 26027.28658252 .00007478 00000-0 34330-3 0 9990
2 63226 97.4132 282.1289 0003516 282.8490 77.2352 15.20687729 48417Epoch: 2026-01-27T06:52Z
TLE epoch observation values (Epoch: 2026-01-27T06:52:40.729Z)
Latitude
-0.0001°
Longitude
52.38905°
Altitude
506.322 km
Speed
7.611 km/s
True Right ascension
18h 48m 30s
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
20:37:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
503.149 km
Perigee altitude
498.312 km
Semi-major axis
6,878.867 km
Eccentricity
0.00035
Inclination
97.4132°
RAAN
282.1289°
Arg. of periapsis
282.849°
True anomaly
77.2745°
Mean anomaly
77.2352°
Eccentric anomaly
77.25485°
Mean motion
3.80424 °/min
Orbital period
94.63 mins
BSTAR
0.0003433
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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 | 2026-01-28 05:32:51.249Z | 19.946° NNE | 2026-01-28 05:35:51.249Z | 77.121° E | 40.952° | 2026-01-28 05:38:51.249Z | 179.486° S |
| 4 mins | 2026-01-28 16:11:51.249Z | 111.304° ESE | 2026-01-28 16:13:51.249Z | 66.432° ENE | 21.962° | 2026-01-28 16:15:51.249Z | 25.229° NE |
| 4 mins | 2026-01-28 17:45:51.249Z | 231.888° WSW | 2026-01-28 17:47:51.249Z | 274.219° WNW | 18.573° | 2026-01-28 17:49:51.249Z | 309.833° NW |
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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