ICEYE-X33, 60548
Orbit data source: Space-Track
ICEYE-X33, 60548 is an American payload satellite in SSO that was launched on Fri, 16 Aug 2024 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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60548 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated 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, 0.8 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ICEYE-X33
1 60548U 24149CJ 25345.22562365 .00008411 00000-0 67945-3 0 9991
2 60548 97.7010 60.8517 0005016 41.3142 318.8461 15.00059926 72011Epoch: 2025-12-11T05:24Z
TLE epoch observation values (Epoch: 2025-12-11T05:24:53.883Z)
Latitude
0.00007°
Longitude
-100.55747°
Altitude
567.143 km
Speed
7.579 km/s
True Right ascension
04h 03m 24s
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
14:06:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.199 km
Perigee altitude
560.235 km
Semi-major axis
6,941.854 km
Eccentricity
0.0005
Inclination
97.701°
RAAN
60.8517°
Arg. of periapsis
41.3142°
True anomaly
318.80826°
Mean anomaly
318.8461°
Eccentric anomaly
318.82718°
Mean motion
3.75258 °/min
Orbital period
95.93 mins
BSTAR
0.00067945
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Other satellites on launch #149 in the year 2024 (2024-08-16 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-X33 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-11 17:12:27.092Z | 51.804° ENE | 2025-12-11 17:14:27.092Z | 84.791° E | 18.632° | 2025-12-11 17:17:27.092Z | 137.944° SSE |
| 4 mins | 2025-12-11 18:48:27.092Z | 326.462° NNW | 2025-12-11 18:50:27.092Z | 275.866° WNW | 25.09° | 2025-12-11 18:52:27.092Z | 238.442° WSW |
| 6 mins | 2025-12-12 05:33:27.092Z | 188.238° SSW | 2025-12-12 05:36:27.092Z | 271.409° WNW | 37.836° | 2025-12-12 05:39:27.092Z | 334.202° NNW |
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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