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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Edit Public Description
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, 0.8 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ICEYE-X40
1 60549U 24149CK 25353.16586468 .00001796 00000-0 16052-3 0 9996
2 60549 97.7002 67.5084 0003831 342.2300 17.8787 14.97138824 73139Epoch: 2025-12-19T03:58Z
TLE epoch observation values (Epoch: 2025-12-19T03:58:50.708Z)
Latitude
-0.00004°
Longitude
-80.2138°
Altitude
576.257 km
Speed
7.574 km/s
True Right ascension
04h 30m 02s
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
19:21:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
575.414 km
Perigee altitude
570.088 km
Semi-major axis
6,950.888 km
Eccentricity
0.00038
Inclination
97.7002°
RAAN
67.5084°
Arg. of periapsis
342.23°
True anomaly
17.89218°
Mean anomaly
17.8787°
Eccentric anomaly
17.88544°
Mean motion
3.74527 °/min
Orbital period
96.12 mins
BSTAR
0.00016052
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-20 04:11:23.849Z | 111.668° ESE | 2025-12-20 04:14:23.849Z | 62.545° ENE | 18.027° | 2025-12-20 04:16:23.849Z | 29.174° NE |
| 5 mins | 2025-12-20 05:47:23.849Z | 218.872° SW | 2025-12-20 05:49:23.849Z | 270.324° WNW | 27.637° | 2025-12-20 05:52:23.849Z | 324.049° NNW |
| 6 mins | 2025-12-20 17:27:23.849Z | 39.994° NE | 2025-12-20 17:30:23.849Z | 108.87° ESE | 28.832° | 2025-12-20 17:33:23.849Z | 160.998° S |
| 4 mins | 2025-12-20 19:03:23.849Z | 321.749° NNW | 2025-12-20 19:05:23.849Z | 285.699° WNW | 17.181° | 2025-12-20 19:07:23.849Z | 254.037° W |
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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