ICEYE-X26, 56961
Orbit data source: Space-Track
ICEYE-X26, 56961 is a payload satellite owned by ICEYE US (US) in SSO that was launched on Mon, 12 Jun 2023 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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56961 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
90 kg wet, 89 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.6 m
Radar Cross Section
0.825 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ICEYE-X26
1 56961U 23084AF 25307.99766918 .00040794 00000-0 50903-3 0 9990
2 56961 97.5724 89.0382 0000636 67.2000 292.9323 15.59777106133839Epoch: 2025-11-03T23:56Z
TLE epoch observation values (Epoch: 2025-11-03T23:56:38.617Z)
Latitude
-0.00003°
Longitude
46.38629°
Altitude
391.273 km
Speed
7.676 km/s
True Right ascension
05h 56m 09s
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
06:26:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
385.652 km
Perigee altitude
384.792 km
Semi-major axis
6,763.359 km
Eccentricity
0.00006
Inclination
97.5724°
RAAN
89.0382°
Arg. of periapsis
67.2°
True anomaly
292.92559°
Mean anomaly
292.9323°
Eccentric anomaly
292.92894°
Mean motion
3.90211 °/min
Orbital period
92.26 mins
BSTAR
0.00050903
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.ICEYE-X26 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-11-04 22:03:51.794Z | 35.904° NE | 2025-11-04 22:05:51.794Z | 93.557° ESE | 30.553° | 2025-11-04 22:07:51.794Z | 159.68° S |
| 4 mins | 2025-11-05 09:57:51.794Z | 210.862° SW | 2025-11-05 09:58:51.794Z | 248.739° W | 31.06° | 2025-11-05 10:01:51.794Z | 330.974° NNW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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