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: 18 hours ago
TLE from 18 hours ago
0 ICEYE-X33
1 60548U 24149CJ 25289.44471864 .00005365 00000-0 44406-3 0 9997
2 60548 97.7109 5.6628 0004666 149.8296 210.3196 14.99294407 63657Epoch: 2025-10-16T10:40Z
TLE epoch observation values (Epoch: 2025-10-16T10:40:23.690Z)
Latitude
-0.00007°
Longitude
-179.64025°
Altitude
574.928 km
Speed
7.572 km/s
True Right ascension
00h 22m 39s
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
23:18:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.322 km
Perigee altitude
562.842 km
Semi-major axis
6,944.219 km
Eccentricity
0.00047
Inclination
97.7109°
RAAN
5.6628°
Arg. of periapsis
149.8296°
True anomaly
210.29262°
Mean anomaly
210.3196°
Eccentric anomaly
210.30611°
Mean motion
3.75066 °/min
Orbital period
95.98 mins
BSTAR
0.00044406
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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 | 2025-10-17 06:01:26.097Z | 216.991° SW | 2025-10-17 06:04:26.097Z | 274.714° WNW | 21.623° | 2025-10-17 06:06:26.097Z | 310.442° NW |
| 6 mins | 2025-10-17 17:41:26.097Z | 35.32° NE | 2025-10-17 17:43:26.097Z | 79.839° E | 33.947° | 2025-10-17 17:47:26.097Z | 170.966° S |
| 5 mins | 2025-10-18 04:28:26.097Z | 112.6° SE | 2025-10-18 04:30:26.097Z | 72.002° E | 23.318° | 2025-10-18 04:33:26.097Z | 17.345° NNE |
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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