ICEYE-X53, 64584
Orbit data source: Space-Track
ICEYE-X53, 64584 is a payload satellite owned by ICEYE (FI) 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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64584 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
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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ICEYE-X53
1 64584U 25135BJ 26297.29420222 .00000529 00000-0 46298-4 0 9991
2 64584 97.7291 53.4286 0001443 157.6579 202.4708 15.00894797 73445Epoch: 2026-10-24T07:03Z
TLE epoch observation values (Epoch: 2026-10-24T07:03:39.071Z)
Latitude
-0.00004°
Longitude
-85.18665°
Altitude
568.117 km
Speed
7.576 km/s
True Right ascension
03h 33m 42s
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
11:13:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.142 km
Perigee altitude
560.14 km
Semi-major axis
6,939.278 km
Eccentricity
0.00014
Inclination
97.7291°
RAAN
53.4286°
Arg. of periapsis
157.6579°
True anomaly
202.46448°
Mean anomaly
202.4708°
Eccentric anomaly
202.46764°
Mean motion
3.75467 °/min
Orbital period
95.88 mins
BSTAR
0.000046298
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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-X53 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 | 2026-10-25 20:25:40.913Z | 25.262° NE | 2026-10-25 20:28:40.913Z | 75.265° E | 47.099° | 2026-10-25 20:32:40.913Z | 174.519° S |
| 5 mins | 2026-10-26 07:12:40.913Z | 118.791° SE | 2026-10-26 07:14:40.913Z | 80.121° E | 27.284° | 2026-10-26 07:17:40.913Z | 18.582° NNE |
| 4 mins | 2026-10-26 08:48:40.913Z | 238.224° WSW | 2026-10-26 08:49:40.913Z | 257.93° W | 20.736° | 2026-10-26 08:52:40.913Z | 311.082° NW |
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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