ICEYE-X54, 64570
Orbit data source: Space-Track
ICEYE-X54, 64570 is a payload satellite owned by RNAF (NL) in SSO that was launched on Mon, 23 Jun 2025 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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64570 intel report (Beta)
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Identifier
Orbit
Country
NL / NETHRelated business
Manufacturer
ICEYE
Mission
Operational Commercial Radar Imaging
Bus & Motor
ICEYE, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 2.4 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X54
1 64570U 25135AU 26289.92132101 .00002820 00000-0 26284-3 0 9991
2 64570 97.7824 43.2697 0001104 262.2889 97.8206 14.95052274 72083Epoch: 2026-10-16T22:06Z
TLE epoch observation values (Epoch: 2026-10-16T22:06:42.135Z)
Latitude
-0.00003°
Longitude
46.15874°
Altitude
585.361 km
Speed
7.568 km/s
True Right ascension
02h 53m 04s
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
02:09:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
579.994 km
Perigee altitude
578.458 km
Semi-major axis
6,957.363 km
Eccentricity
0.00011
Inclination
97.7824°
RAAN
43.2697°
Arg. of periapsis
262.2889°
True anomaly
97.83313°
Mean anomaly
97.8206°
Eccentric anomaly
97.82687°
Mean motion
3.74004 °/min
Orbital period
96.26 mins
BSTAR
0.00026284
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Other satellites on launch #135 in the year 2025 (2025-06-23 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-X54 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-10-17 07:51:52.214Z | 175.447° S | 2026-10-17 07:55:52.214Z | 286.294° WNW | 66.163° | 2026-10-17 07:58:52.214Z | 340.546° N |
| 4 mins | 2026-10-17 19:35:52.214Z | 66.16° ENE | 2026-10-17 19:37:52.214Z | 101.624° ESE | 17.455° | 2026-10-17 19:39:52.214Z | 132.539° SE |
| 5 mins | 2026-10-17 21:10:52.214Z | 337.816° N | 2026-10-17 21:12:52.214Z | 288.764° WNW | 34.414° | 2026-10-17 21:15:52.214Z | 228.648° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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