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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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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X25
1 56963U 23084AH 25363.83840578 .00056301 00000-0 12097-2 0 9994
2 56963 97.5750 135.6012 0005757 196.6280 163.4779 15.44477373141691Epoch: 2025-12-29T20:07Z
TLE epoch observation values (Epoch: 2025-12-29T20:07:18.259Z)
Latitude
-0.00012°
Longitude
95.24485°
Altitude
439.793 km
Speed
7.646 km/s
True Right ascension
09h 02m 24s
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
03:28:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
433.774 km
Perigee altitude
425.935 km
Semi-major axis
6,807.992 km
Eccentricity
0.00058
Inclination
97.575°
RAAN
135.6012°
Arg. of periapsis
196.628°
True anomaly
163.49665°
Mean anomaly
163.4779°
Eccentric anomaly
163.48728°
Mean motion
3.8638 °/min
Orbital period
93.17 mins
BSTAR
0.0012097
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-30 08:41:52.348Z | 143.552° SSE | 2025-12-30 08:43:52.348Z | 100.439° ESE | 33.548° | 2025-12-30 08:46:52.348Z | 4.358° NNE |
| 4 mins | 2025-12-30 21:34:52.348Z | 40.602° NE | 2025-12-30 21:35:52.348Z | 71.944° E | 33.767° | 2025-12-30 21:38:52.348Z | 171.105° S |
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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