ICEYE-X43, 60539
Orbit data source: Space-Track
ICEYE-X43, 60539 is a Brazilian payload satellite 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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Edit Public Description
Identifier
Orbit
Country
Unknown / BRAZRelated 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: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X43
1 60539U 24149BZ 26035.17025794 .00004853 00000-0 40439-3 0 9997
2 60539 97.6925 113.9274 0004802 124.0524 236.1155 14.99081843 80189Epoch: 2026-02-04T04:05Z
TLE epoch observation values (Epoch: 2026-02-04T04:05:10.286Z)
Latitude
-0.00003°
Longitude
-81.70614°
Altitude
574.647 km
Speed
7.572 km/s
True Right ascension
07h 35m 42s
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
12:25:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.073 km
Perigee altitude
563.403 km
Semi-major axis
6,944.875 km
Eccentricity
0.00048
Inclination
97.6925°
RAAN
113.9274°
Arg. of periapsis
124.0524°
True anomaly
236.06983°
Mean anomaly
236.1155°
Eccentric anomaly
236.09267°
Mean motion
3.75013 °/min
Orbital period
96 mins
BSTAR
0.00040439
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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 | 2026-02-04 17:28:13.257Z | 32.585° NE | 2026-02-04 17:31:13.257Z | 82.89° E | 28.964° | 2026-02-04 17:35:13.257Z | 163.576° S |
| 4 mins | 2026-02-05 04:17:13.257Z | 94.278° ESE | 2026-02-05 04:18:13.257Z | 74.621° E | 19.383° | 2026-02-05 04:21:13.257Z | 22.663° NE |
| 5 mins | 2026-02-05 05:51:13.257Z | 215.373° SW | 2026-02-05 05:53:13.257Z | 256.867° W | 25.38° | 2026-02-05 05:56:13.257Z | 317.726° NNW |
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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