ICEYE-X39, 60546
Orbit data source: Space-Track
ICEYE-X39, 60546 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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60546 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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X39
1 60546U 24149CG 26265.73293803 .00001457 00000-0 12182-3 0 9991
2 60546 97.6709 341.4689 0010026 165.9513 194.1992 15.00014698114741Epoch: 2026-09-22T17:35Z
TLE epoch observation values (Epoch: 2026-09-22T17:35:25.845Z)
Latitude
0.00003°
Longitude
76.01703°
Altitude
576.659 km
Speed
7.569 km/s
True Right ascension
22h 45m 52s
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
22:14:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
570.815 km
Perigee altitude
556.895 km
Semi-major axis
6,941.992 km
Eccentricity
0.001
Inclination
97.6709°
RAAN
341.4689°
Arg. of periapsis
165.9513°
True anomaly
194.17105°
Mean anomaly
194.1992°
Eccentric anomaly
194.18512°
Mean motion
3.75247 °/min
Orbital period
95.94 mins
BSTAR
0.00012182
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-23 18:10:36.283Z | 6.029° NNE | 2026-09-23 18:13:36.283Z | 266.128° W | 71.641° | 2026-09-23 18:16:36.283Z | 201.509° SSW |
| 6 mins | 2026-09-24 04:57:36.283Z | 144.928° SSE | 2026-09-24 04:59:36.283Z | 77.235° E | 59.529° | 2026-09-24 05:03:36.283Z | 355.644° N |
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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