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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X26
1 56961U 23084AF 25320.69511330 .00051118 00000-0 60609-3 0 9994
2 56961 97.5726 102.5866 0000423 35.3763 324.7522 15.61071423135812Epoch: 2025-11-16T16:40Z
TLE epoch observation values (Epoch: 2025-11-16T16:40:57.789Z)
Latitude
0.00002°
Longitude
156.33959°
Altitude
387.468 km
Speed
7.678 km/s
True Right ascension
06h 50m 20s
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
21:38:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
381.766 km
Perigee altitude
381.194 km
Semi-major axis
6,759.617 km
Eccentricity
0.00004
Inclination
97.5726°
RAAN
102.5866°
Arg. of periapsis
35.3763°
True anomaly
324.7494°
Mean anomaly
324.7522°
Eccentric anomaly
324.7508°
Mean motion
3.90535 °/min
Orbital period
92.18 mins
BSTAR
0.00060609
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-11-17 09:44:23.501Z | 174.138° S | 2025-11-17 09:46:23.501Z | 224.145° SW | 43.333° | 2025-11-17 09:49:23.501Z | 343.854° N |
| 4 mins | 2025-11-17 22:29:23.501Z | 17.595° NNE | 2025-11-17 22:30:23.501Z | 59.863° ENE | 44.58° | 2025-11-17 22:33:23.501Z | 190.663° SSW |
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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