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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X54
1 64570U 25135AU 26224.59268622 .00001485 00000-0 14181-3 0 9990
2 64570 97.7765 338.4886 0003871 119.1375 241.0234 14.94795198 62327Epoch: 2026-08-12T14:13Z
TLE epoch observation values (Epoch: 2026-08-12T14:13:28.089Z)
Latitude
0.00006°
Longitude
164.07715°
Altitude
587.36 km
Speed
7.566 km/s
True Right ascension
22h 33m 57s
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
16:55:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.718 km
Perigee altitude
577.331 km
Semi-major axis
6,958.161 km
Eccentricity
0.00039
Inclination
97.7765°
RAAN
338.4886°
Arg. of periapsis
119.1375°
True anomaly
240.9846°
Mean anomaly
241.0234°
Eccentric anomaly
241.004°
Mean motion
3.7394 °/min
Orbital period
96.27 mins
BSTAR
0.00014181
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-08-13 08:01:28.688Z | 188.999° SSW | 2026-08-13 08:04:28.688Z | 266.249° W | 37.598° | 2026-08-13 08:07:28.688Z | 332.733° NNW |
| 5 mins | 2026-08-13 19:44:28.688Z | 58.954° ENE | 2026-08-13 19:46:28.688Z | 99.027° ESE | 21.084° | 2026-08-13 19:49:28.688Z | 147.353° SSE |
| 5 mins | 2026-08-13 21:19:28.688Z | 334.426° NNW | 2026-08-13 21:21:28.688Z | 294.199° NW | 23.958° | 2026-08-13 21:24:28.688Z | 238.21° 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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