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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X40
1 60549U 24149CK 25297.75437530 .00002532 00000-0 22574-3 0 9998
2 60549 97.7041 12.9244 0005932 136.6295 223.5394 14.96867407 64849Epoch: 2025-10-24T18:06Z
TLE epoch observation values (Epoch: 2025-10-24T18:06:18.025Z)
Latitude
-0.00009°
Longitude
67.95457°
Altitude
582.625 km
Speed
7.567 km/s
True Right ascension
00h 51m 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
19:58:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
577.716 km
Perigee altitude
569.468 km
Semi-major axis
6,951.729 km
Eccentricity
0.00059
Inclination
97.7041°
RAAN
12.9244°
Arg. of periapsis
136.6295°
True anomaly
223.4926°
Mean anomaly
223.5394°
Eccentric anomaly
223.516°
Mean motion
3.74459 °/min
Orbital period
96.14 mins
BSTAR
0.00022574
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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 | 2025-10-25 05:28:18.683Z | 190.197° SSW | 2025-10-25 05:30:18.683Z | 236.526° WSW | 37.941° | 2025-10-25 05:34:18.683Z | 336.67° NNW |
| 4 mins | 2025-10-25 17:10:18.683Z | 67.625° E | 2025-10-25 17:11:18.683Z | 87.2° E | 19.481° | 2025-10-25 17:14:18.683Z | 140.132° SSE |
| 5 mins | 2025-10-25 18:45:18.683Z | 326.962° NNW | 2025-10-25 18:47:18.683Z | 278.382° WNW | 24.687° | 2025-10-25 18:50:18.683Z | 231.071° 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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