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: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X53
1 64584U 25135BJ 26207.62529053 .00003845 00000-0 30634-3 0 9991
2 64584 97.7348 324.2298 0002387 161.4121 198.7190 15.00952425 59993Epoch: 2026-07-26T15:00Z
TLE epoch observation values (Epoch: 2026-07-26T15:00:25.101Z)
Latitude
-0.00008°
Longitude
154.80469°
Altitude
568.583 km
Speed
7.576 km/s
True Right ascension
21h 36m 55s
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
17:28:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.62 km
Perigee altitude
559.307 km
Semi-major axis
6,939.101 km
Eccentricity
0.00024
Inclination
97.7348°
RAAN
324.2298°
Arg. of periapsis
161.4121°
True anomaly
198.71022°
Mean anomaly
198.719°
Eccentric anomaly
198.71461°
Mean motion
3.75481 °/min
Orbital period
95.88 mins
BSTAR
0.00030634
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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 | 2026-07-27 07:08:25.423Z | 128.227° SE | 2026-07-27 07:11:25.423Z | 79.084° E | 24.628° | 2026-07-27 07:14:25.423Z | 18.049° NNE |
| 4 mins | 2026-07-27 08:45:25.423Z | 238.998° WSW | 2026-07-27 08:46:25.423Z | 258.853° W | 19.392° | 2026-07-27 08:49:25.423Z | 311.533° NW |
| 6 mins | 2026-07-27 20:23:25.423Z | 32.446° NE | 2026-07-27 20:25:25.423Z | 79.311° E | 36.399° | 2026-07-27 20:29:25.423Z | 174.769° S |
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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