ICEYE-X40, 60549
Orbit data source: Space-Track
ICEYE-X40, 60549 is a payload satellite owned by Yahsat (AE) 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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60549 intel report (Beta)
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Identifier
Orbit
Country
AE / UAERelated 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ICEYE-X40
1 60549U 24149CK 26312.02093264 .00005799 00000-0 48700-3 0 9996
2 60549 97.6690 26.1740 0002866 329.2607 30.8448 14.98700716121615Epoch: 2026-11-08T00:30Z
TLE epoch observation values (Epoch: 2026-11-08T00:30:08.580Z)
Latitude
0.00005°
Longitude
-28.57958°
Altitude
572.253 km
Speed
7.576 km/s
True Right ascension
01h 44m 41s
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
23:36:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.906 km
Perigee altitude
565.925 km
Semi-major axis
6,946.052 km
Eccentricity
0.00029
Inclination
97.669°
RAAN
26.174°
Arg. of periapsis
329.2607°
True anomaly
30.86164°
Mean anomaly
30.8448°
Eccentric anomaly
30.85322°
Mean motion
3.74918 °/min
Orbital period
96.02 mins
BSTAR
0.000487
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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-X40 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 | 2026-11-09 05:28:28.074Z | 190.485° SSW | 2026-11-09 05:31:28.074Z | 273.85° WNW | 48.762° | 2026-11-09 05:34:28.074Z | 333.426° NNW |
| 5 mins | 2026-11-09 17:09:28.074Z | 57.471° ENE | 2026-11-09 17:11:28.074Z | 96.468° ESE | 22.302° | 2026-11-09 17:14:28.074Z | 145.907° SSE |
| 5 mins | 2026-11-09 18:44:28.074Z | 332.824° NNW | 2026-11-09 18:46:28.074Z | 290.676° WNW | 26.74° | 2026-11-09 18:49:28.074Z | 236.343° WSW |
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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