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: 2 days ago
TLE from 2 days ago
0 ICEYE-X26
1 56961U 23084AF 25312.35959750 .00045389 00000-0 55735-3 0 9997
2 56961 97.5738 93.6903 0000575 60.8065 299.3249 15.60177963134517Epoch: 2025-11-08T08:37Z
TLE epoch observation values (Epoch: 2025-11-08T08:37:49.223Z)
Latitude
-0.00004°
Longitude
-83.55513°
Altitude
390.092 km
Speed
7.676 km/s
True Right ascension
06h 14m 45s
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
20:46:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
384.451 km
Perigee altitude
383.674 km
Semi-major axis
6,762.199 km
Eccentricity
0.00006
Inclination
97.5738°
RAAN
93.6903°
Arg. of periapsis
60.8065°
True anomaly
299.31916°
Mean anomaly
299.3249°
Eccentric anomaly
299.32203°
Mean motion
3.90311 °/min
Orbital period
92.23 mins
BSTAR
0.00055735
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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 | 2025-11-10 10:01:17.727Z | 202.079° SSW | 2025-11-10 10:03:17.727Z | 266.141° W | 29.327° | 2025-11-10 10:05:17.727Z | 322.78° NNW |
| 4 mins | 2025-11-10 22:46:17.727Z | 340.099° N | 2025-11-10 22:47:17.727Z | 296.189° NW | 34.937° | 2025-11-10 22:50:17.727Z | 211.555° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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