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: 22 hours ago
TLE from 22 hours ago
0 ICEYE-X33
1 60548U 24149CJ 26276.49832420 .00002389 00000-0 19064-3 0 9993
2 60548 97.7520 355.2389 0001490 68.0636 292.0746 15.01256979116455Epoch: 2026-10-03T11:57Z
TLE epoch observation values (Epoch: 2026-10-03T11:57:35.210Z)
Latitude
-0.00007°
Longitude
163.63714°
Altitude
565.685 km
Speed
7.579 km/s
True Right ascension
23h 40m 57s
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
04:17:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.059 km
Perigee altitude
558.991 km
Semi-major axis
6,938.162 km
Eccentricity
0.00015
Inclination
97.752°
RAAN
355.2389°
Arg. of periapsis
68.0636°
True anomaly
292.05878°
Mean anomaly
292.0746°
Eccentric anomaly
292.06669°
Mean motion
3.75558 °/min
Orbital period
95.86 mins
BSTAR
0.00019064
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-10-04 17:20:46.928Z | 57.403° ENE | 2026-10-04 17:22:46.928Z | 92.727° ESE | 19.208° | 2026-10-04 17:24:46.928Z | 129.007° SE |
| 5 mins | 2026-10-04 18:55:46.928Z | 336.261° NNW | 2026-10-04 18:57:46.928Z | 291.235° WNW | 30.039° | 2026-10-04 19:00:46.928Z | 232.566° WSW |
| 6 mins | 2026-10-05 05:40:46.928Z | 186.01° SSW | 2026-10-05 05:43:46.928Z | 273.692° WNW | 54.238° | 2026-10-05 05:46:46.928Z | 335.657° 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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