ICEYE-X43, 60539
Orbit data source: Space-Track
ICEYE-X43, 60539 is a payload satellite owned by ICEYE 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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60539 intel report (Beta)
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Identifier
Orbit
Country
FIRelated 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, 1.4 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-X43
1 60539U 24149BZ 26304.18712319 .00000921 00000-0 78421-4 0 9998
2 60539 97.6695 19.2577 0009448 297.8061 62.2204 15.00178789120506Epoch: 2026-10-31T04:29Z
TLE epoch observation values (Epoch: 2026-10-31T04:29:27.443Z)
Latitude
-0.00008°
Longitude
-87.60308°
Altitude
566.347 km
Speed
7.58 km/s
True Right ascension
01h 17m 01s
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
02:18:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.907 km
Perigee altitude
556.79 km
Semi-major axis
6,941.485 km
Eccentricity
0.00094
Inclination
97.6695°
RAAN
19.2577°
Arg. of periapsis
297.8061°
True anomaly
62.31624°
Mean anomaly
62.2204°
Eccentric anomaly
62.26832°
Mean motion
3.75288 °/min
Orbital period
95.93 mins
BSTAR
0.000078421
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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-X43 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-11-01 17:52:12.194Z | 17.691° NNE | 2026-11-01 17:56:12.194Z | 129.077° SE | 67.158° | 2026-11-01 17:59:12.194Z | 183.813° SSW |
| 5 mins | 2026-11-02 04:40:12.194Z | 121.592° SE | 2026-11-02 04:42:12.194Z | 66.359° ENE | 36.548° | 2026-11-02 04:45:12.194Z | 8.61° NNE |
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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