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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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: 1 day ago
TLE from 1 day ago
0 ICEYE-X33
1 60548U 24149CJ 26259.16814932 .00003880 00000-0 30745-3 0 9992
2 60548 97.7494 337.9474 0001173 55.3364 304.7971 15.01158259113856Epoch: 2026-09-16T04:02Z
TLE epoch observation values (Epoch: 2026-09-16T04:02:08.101Z)
Latitude
0.00006°
Longitude
-77.70998°
Altitude
565.914 km
Speed
7.578 km/s
True Right ascension
22h 31m 47s
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
03:01:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.143 km
Perigee altitude
559.516 km
Semi-major axis
6,938.466 km
Eccentricity
0.00012
Inclination
97.7494°
RAAN
337.9474°
Arg. of periapsis
55.3364°
True anomaly
304.78606°
Mean anomaly
304.7971°
Eccentric anomaly
304.79158°
Mean motion
3.75533 °/min
Orbital period
95.86 mins
BSTAR
0.00030745
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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 | 2026-09-17 17:24:54.069Z | 49.696° ENE | 2026-09-17 17:27:54.069Z | 105.811° ESE | 21.563° | 2026-09-17 17:29:54.069Z | 139.931° SSE |
| 4 mins | 2026-09-17 19:00:54.069Z | 323.744° NNW | 2026-09-17 19:01:54.069Z | 301.795° NW | 25.749° | 2026-09-17 19:04:54.069Z | 240.703° WSW |
| 6 mins | 2026-09-18 05:45:54.069Z | 196.467° SSW | 2026-09-18 05:47:54.069Z | 247.695° W | 46.133° | 2026-09-18 05:51:54.069Z | 334.843° 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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