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: 11 hours ago
TLE from 11 hours ago
0 ETIHAD-SAT
1 63226U 25052S 25334.63005135 .00005654 00000-0 26602-3 0 9992
2 63226 97.4165 225.4242 0007046 109.5890 250.6107 15.19931181 39656Epoch: 2025-11-30T15:07Z
TLE epoch observation values (Epoch: 2025-11-30T15:07:16.436Z)
Latitude
0.00004°
Longitude
-71.13544°
Altitude
510.752 km
Speed
7.608 km/s
True Right ascension
15h 01m 41s
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
00:14:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.863 km
Perigee altitude
498.166 km
Semi-major axis
6,881.152 km
Eccentricity
0.0007
Inclination
97.4165°
RAAN
225.4242°
Arg. of periapsis
109.589°
True anomaly
250.53456°
Mean anomaly
250.6107°
Eccentric anomaly
250.57263°
Mean motion
3.80234 °/min
Orbital period
94.68 mins
BSTAR
0.00026602
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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 | 2025-12-01 05:53:49.097Z | 5.849° NNE | 2025-12-01 05:56:49.097Z | 316.756° NNW | 41.982° | 2025-12-01 05:59:49.097Z | 203.439° SW |
| 5 mins | 2025-12-01 16:32:49.097Z | 135.775° SSE | 2025-12-01 16:34:49.097Z | 81.399° E | 34.011° | 2025-12-01 16:37:49.097Z | 5.767° NNE |
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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