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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ICEYE-X25 radio frequencies
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Edit Public Description
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, 1.6 m
Radar Cross Section
0.825 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 ICEYE-X25
1 56963U 23084AH 25261.31936330 .00023680 00000-0 67451-3 0 9995
2 56963 97.5725 29.4375 0007535 198.4399 161.6572 15.36072592125915Epoch: 2025-09-18T07:39Z
TLE epoch observation values (Epoch: 2025-09-18T07:39:52.989Z)
Latitude
-0.00004°
Longitude
-83.01595°
Altitude
465.734 km
Speed
7.631 km/s
True Right ascension
01h 57m 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
20:09:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
459.837 km
Perigee altitude
449.54 km
Semi-major axis
6,832.825 km
Eccentricity
0.00075
Inclination
97.5725°
RAAN
29.4375°
Arg. of periapsis
198.4399°
True anomaly
161.68435°
Mean anomaly
161.6572°
Eccentric anomaly
161.67078°
Mean motion
3.84276 °/min
Orbital period
93.68 mins
BSTAR
0.00067451
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-19 08:48:12.905Z | 175.802° S | 2025-09-19 08:51:12.905Z | 265.553° W | 42.833° | 2025-09-19 08:54:12.905Z | 341.751° N |
| 5 mins | 2025-09-19 21:45:12.905Z | 358.041° N | 2025-09-19 21:47:12.905Z | 300.702° NW | 39.381° | 2025-09-19 21:50:12.905Z | 208.027° 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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