ICEYE-X25, 56963
Orbit data source: Space-Track
ICEYE-X25, 56963 is a payload satellite owned by ICEYE (FI) 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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56963 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated 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, 2.4 m
Radar Cross Section
0.825 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X25
1 56963U 23084AH 26063.16602668 .00076637 00000-0 13104-2 0 9998
2 56963 97.5761 202.9833 0003906 300.8681 59.2186 15.51005364151645Epoch: 2026-03-04T03:59Z
TLE epoch observation values (Epoch: 2026-03-04T03:59:04.705Z)
Latitude
0.00001°
Longitude
-18.72094°
Altitude
415.56 km
Speed
7.662 km/s
True Right ascension
13h 31m 55s
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
15:06:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
413.373 km
Perigee altitude
408.07 km
Semi-major axis
6,788.859 km
Eccentricity
0.00039
Inclination
97.5761°
RAAN
202.9833°
Arg. of periapsis
300.8681°
True anomaly
59.25706°
Mean anomaly
59.2186°
Eccentric anomaly
59.23783°
Mean motion
3.88015 °/min
Orbital period
92.78 mins
BSTAR
0.0013104
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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-X25 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 | 2026-03-04 21:35:32.731Z | 49.776° ENE | 2026-03-04 21:37:32.731Z | 106.425° ESE | 24.003° | 2026-03-04 21:39:32.731Z | 152.413° SSE |
| 4 mins | 2026-03-05 09:32:32.731Z | 190.885° SSW | 2026-03-05 09:34:32.731Z | 273.282° WNW | 37.355° | 2026-03-05 09:36:32.731Z | 331.802° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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