ICEYE-X39, 60546
Orbit data source: Space-Track
ICEYE-X39, 60546 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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60546 intel report (Beta)
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Identifier
Orbit
Country
BR / 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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X39
1 60546U 24149CG 26171.21245838 .00002346 00000-0 19379-3 0 9998
2 60546 97.6757 248.1948 0005642 110.8245 249.3583 14.99909996100570Epoch: 2026-06-20T05:05Z
TLE epoch observation values (Epoch: 2026-06-20T05:05:56.404Z)
Latitude
-0.00001°
Longitude
-96.72054°
Altitude
571.613 km
Speed
7.574 km/s
True Right ascension
16h 32m 46s
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
07:23:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
568.095 km
Perigee altitude
560.262 km
Semi-major axis
6,942.315 km
Eccentricity
0.00056
Inclination
97.6757°
RAAN
248.1948°
Arg. of periapsis
110.8245°
True anomaly
249.29781°
Mean anomaly
249.3583°
Eccentric anomaly
249.32805°
Mean motion
3.75221 °/min
Orbital period
95.94 mins
BSTAR
0.00019379
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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-X39 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 | 2026-06-21 05:13:51.158Z | 170.114° S | 2026-06-21 05:17:51.158Z | 308.492° NW | 44.126° | 2026-06-21 05:20:51.158Z | 344.895° N |
| 6 mins | 2026-06-21 18:29:51.158Z | 348.482° N | 2026-06-21 18:31:51.158Z | 305.561° NW | 32.573° | 2026-06-21 18:35:51.158Z | 217.832° SW |
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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