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: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X53
1 64584U 25135BJ 26083.55518683 .00005298 00000-0 42070-3 0 9993
2 64584 97.7416 200.6757 0001936 184.6642 175.4564 15.00904203 41382Epoch: 2026-03-24T13:19Z
TLE epoch observation values (Epoch: 2026-03-24T13:19:28.142Z)
Latitude
-0.00001°
Longitude
178.77728°
Altitude
568.501 km
Speed
7.576 km/s
True Right ascension
13h 22m 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
00:43:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.456 km
Perigee altitude
559.769 km
Semi-major axis
6,939.25 km
Eccentricity
0.00019
Inclination
97.7416°
RAAN
200.6757°
Arg. of periapsis
184.6642°
True anomaly
175.45816°
Mean anomaly
175.4564°
Eccentric anomaly
175.45728°
Mean motion
3.75469 °/min
Orbital period
95.88 mins
BSTAR
0.0004207
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-03-24 20:18:00.358Z | 28.464° NE | 2026-03-24 20:21:00.358Z | 106.219° ESE | 37.257° | 2026-03-24 20:24:00.358Z | 172.414° S |
| 5 mins | 2026-03-25 07:05:00.358Z | 111.577° ESE | 2026-03-25 07:07:00.358Z | 65.339° ENE | 24.906° | 2026-03-25 07:10:00.358Z | 13.328° NNE |
| 4 mins | 2026-03-25 08:40:00.358Z | 230.865° WSW | 2026-03-25 08:42:00.358Z | 269.635° W | 19.412° | 2026-03-25 08:44:00.358Z | 305.408° 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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