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: 8 hours ago
TLE from 8 hours ago
0 ICEYE-X53
1 64584U 25135BJ 26133.28997228 .00001716 00000-0 13972-3 0 9995
2 64584 97.7404 250.2182 0001984 132.0925 228.0467 15.00853583 48845Epoch: 2026-05-13T06:57Z
TLE epoch observation values (Epoch: 2026-05-13T06:57:33.604Z)
Latitude
-0.00007°
Longitude
-85.22393°
Altitude
568.239 km
Speed
7.576 km/s
True Right ascension
16h 40m 52s
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
22:53:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.646 km
Perigee altitude
559.892 km
Semi-major axis
6,939.406 km
Eccentricity
0.0002
Inclination
97.7404°
RAAN
250.2182°
Arg. of periapsis
132.0925°
True anomaly
228.0298°
Mean anomaly
228.0467°
Eccentric anomaly
228.03825°
Mean motion
3.75457 °/min
Orbital period
95.88 mins
BSTAR
0.00013972
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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 | 2026-05-13 20:19:25.776Z | 24.715° NE | 2026-05-13 20:23:25.776Z | 122.453° SE | 36.324° | 2026-05-13 20:26:25.776Z | 174.035° S |
| 4 mins | 2026-05-14 07:07:25.776Z | 106.982° ESE | 2026-05-14 07:09:25.776Z | 57.819° ENE | 24.467° | 2026-05-14 07:11:25.776Z | 20.342° NNE |
| 4 mins | 2026-05-14 08:42:25.776Z | 235.211° WSW | 2026-05-14 08:44:25.776Z | 275.474° WNW | 19.076° | 2026-05-14 08:46:25.776Z | 308.83° 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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