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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X40
1 60549U 24149CK 26260.20525046 .00002791 00000-0 23876-3 0 9992
2 60549 97.6722 335.2166 0005452 125.7774 234.3956 14.98403986113856Epoch: 2026-09-17T04:55Z
TLE epoch observation values (Epoch: 2026-09-17T04:55:33.639Z)
Latitude
-0.00006°
Longitude
-94.81939°
Altitude
577.088 km
Speed
7.571 km/s
True Right ascension
22h 20m 51s
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
09:30:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.621 km
Perigee altitude
565.046 km
Semi-major axis
6,946.97 km
Eccentricity
0.00055
Inclination
97.6722°
RAAN
335.2166°
Arg. of periapsis
125.7774°
True anomaly
234.34482°
Mean anomaly
234.3956°
Eccentric anomaly
234.37021°
Mean motion
3.74844 °/min
Orbital period
96.04 mins
BSTAR
0.00023876
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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 | 2026-09-17 18:19:14.045Z | 355.765° N | 2026-09-17 18:22:14.045Z | 266.074° W | 49.833° | 2026-09-17 18:25:14.045Z | 212.233° SW |
| 6 mins | 2026-09-18 05:06:14.045Z | 163.833° S | 2026-09-18 05:09:14.045Z | 359.773° N | 67.946° | 2026-09-18 05:12:14.045Z | 349.205° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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