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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X40
1 60549U 24149CK 26264.74621356 .00002260 00000-0 19414-3 0 9990
2 60549 97.6723 339.6820 0005954 113.4697 246.7152 14.98423762114532Epoch: 2026-09-21T17:54Z
TLE epoch observation values (Epoch: 2026-09-21T17:54:32.851Z)
Latitude
-0.00003°
Longitude
70.4235°
Altitude
576.457 km
Speed
7.572 km/s
True Right ascension
22h 38m 43s
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
02:01:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.908 km
Perigee altitude
564.636 km
Semi-major axis
6,946.909 km
Eccentricity
0.0006
Inclination
97.6723°
RAAN
339.682°
Arg. of periapsis
113.4697°
True anomaly
246.65255°
Mean anomaly
246.7152°
Eccentric anomaly
246.68387°
Mean motion
3.74848 °/min
Orbital period
96.04 mins
BSTAR
0.00019414
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-22 16:56:45.003Z | 63.801° ENE | 2026-09-22 16:58:45.003Z | 97.002° ESE | 15.705° | 2026-09-22 17:00:45.003Z | 128.009° SE |
| 5 mins | 2026-09-22 18:31:45.003Z | 340.742° N | 2026-09-22 18:33:45.003Z | 289.748° WNW | 37.029° | 2026-09-22 18:36:45.003Z | 225.687° WSW |
| 7 mins | 2026-09-23 05:17:45.003Z | 177.531° S | 2026-09-23 05:20:45.003Z | 264.648° W | 68.493° | 2026-09-23 05:24:45.003Z | 342.66° N |
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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