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 26005.36585223 .00053427 00000-0 52771-3 0 9997
2 56961 97.5731 155.8200 0000609 105.6455 254.4872 15.65747199143579Epoch: 2026-01-05T08:46Z
TLE epoch observation values (Epoch: 2026-01-05T08:46:49.632Z)
Latitude
0.00001°
Longitude
-80.85085°
Altitude
374.348 km
Speed
7.685 km/s
True Right ascension
10h 23m 16s
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
04:04:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
368.414 km
Perigee altitude
367.592 km
Semi-major axis
6,746.14 km
Eccentricity
0.00006
Inclination
97.5731°
RAAN
155.82°
Arg. of periapsis
105.6455°
True anomaly
254.48048°
Mean anomaly
254.4872°
Eccentric anomaly
254.48384°
Mean motion
3.91706 °/min
Orbital period
91.91 mins
BSTAR
0.00052771
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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 | 2026-01-07 09:59:00.848Z | 169.955° S | 2026-01-07 10:02:00.848Z | 313.69° NW | 43.871° | 2026-01-07 10:04:00.848Z | 344.843° N |
| 4 mins | 2026-01-07 22:42:00.848Z | 24.389° NE | 2026-01-07 22:43:00.848Z | 49.917° ENE | 39.681° | 2026-01-07 22:46:00.848Z | 184.723° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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