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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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, 0.8 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 14 hours ago
TLE from 14 hours ago
0 ICEYE-X39
1 60546U 24149CG 25289.15705904 .00005325 00000-0 45857-3 0 9995
2 60546 97.7034 4.4558 0005007 159.6038 200.5385 14.97759180 63567Epoch: 2025-10-16T03:46Z
TLE epoch observation values (Epoch: 2025-10-16T03:46:09.901Z)
Latitude
0°
Longitude
-77.00627°
Altitude
580.134 km
Speed
7.569 km/s
True Right ascension
00h 17m 49s
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
12:32:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
574.309 km
Perigee altitude
567.351 km
Semi-major axis
6,948.967 km
Eccentricity
0.0005
Inclination
97.7034°
RAAN
4.4558°
Arg. of periapsis
159.6038°
True anomaly
200.51838°
Mean anomaly
200.5385°
Eccentric anomaly
200.52844°
Mean motion
3.74682 °/min
Orbital period
96.08 mins
BSTAR
0.00045857
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-10-16 18:46:09.242Z | 339.001° N | 2025-10-16 18:48:09.242Z | 302.684° NW | 23.675° | 2025-10-16 18:51:09.242Z | 240.749° WSW |
| 6 mins | 2025-10-17 05:33:09.242Z | 192.879° SSW | 2025-10-17 05:36:09.242Z | 270.95° WNW | 35.523° | 2025-10-17 05:39:09.242Z | 331.505° NNW |
| 4 mins | 2025-10-17 17:15:09.242Z | 65.92° ENE | 2025-10-17 17:16:09.242Z | 86.997° E | 21.56° | 2025-10-17 17:19:09.242Z | 143.54° SSE |
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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