ICEYE-X45, 62705
Orbit data source: Space-Track
ICEYE-X45, 62705 is a payload satellite owned by ICEYE US (US) in SSO that was launched on Tue, 14 Jan 2025 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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62705 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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: 17 hours ago
TLE from 17 hours ago
0 ICEYE-X45
1 62705U 25009DA 26307.20423264 .00004371 00000-0 34727-3 0 9998
2 62705 97.8687 35.2818 0000756 87.4926 272.6384 15.01001271 98533Epoch: 2026-11-03T04:54Z
TLE epoch observation values (Epoch: 2026-11-03T04:54:05.700Z)
Latitude
-0°
Longitude
-80.71221°
Altitude
566.834 km
Speed
7.578 km/s
True Right ascension
02h 21m 07s
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
18:09:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
561.343 km
Perigee altitude
560.294 km
Semi-major axis
6,938.956 km
Eccentricity
0.00008
Inclination
97.8687°
RAAN
35.2818°
Arg. of periapsis
87.4926°
True anomaly
272.62975°
Mean anomaly
272.6384°
Eccentric anomaly
272.63407°
Mean motion
3.75493 °/min
Orbital period
95.87 mins
BSTAR
0.00034727
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Other satellites on launch #9 in the year 2025 (2025-01-14 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-X45 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 | 2026-11-04 05:03:20.902Z | 105.907° ESE | 2026-11-04 05:05:20.902Z | 73.554° E | 18.105° | 2026-11-04 05:08:20.902Z | 24.401° NE |
| 5 mins | 2026-11-04 06:38:20.902Z | 212.498° SW | 2026-11-04 06:40:20.902Z | 260.554° W | 32.9° | 2026-11-04 06:43:20.902Z | 322.262° NNW |
| 5 mins | 2026-11-04 18:17:20.902Z | 48.067° ENE | 2026-11-04 18:19:20.902Z | 91.095° ESE | 29.64° | 2026-11-04 18:22:20.902Z | 152.838° 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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