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, 0.6 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 ICEYE-X45
1 62705U 25009DA 26171.19634949 .00002266 00000-0 18314-3 0 9994
2 62705 97.8328 257.9063 0001248 94.2462 265.8904 15.00840975 78135Epoch: 2026-06-20T04:42Z
TLE epoch observation values (Epoch: 2026-06-20T04:42:44.595Z)
Latitude
-0.00006°
Longitude
-81.19395°
Altitude
567.416 km
Speed
7.577 km/s
True Right ascension
17h 11m 37s
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
07:23:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.178 km
Perigee altitude
560.446 km
Semi-major axis
6,939.449 km
Eccentricity
0.00012
Inclination
97.8328°
RAAN
257.9063°
Arg. of periapsis
94.2462°
True anomaly
265.87614°
Mean anomaly
265.8904°
Eccentric anomaly
265.88327°
Mean motion
3.75453 °/min
Orbital period
95.88 mins
BSTAR
0.00018314
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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 | 2026-06-21 04:51:43.406Z | 111.896° ESE | 2026-06-21 04:54:43.406Z | 62.145° ENE | 17.966° | 2026-06-21 04:56:43.406Z | 28.54° NE |
| 6 mins | 2026-06-21 06:26:43.406Z | 208.778° SW | 2026-06-21 06:29:43.406Z | 277.613° WNW | 26.547° | 2026-06-21 06:32:43.406Z | 325.624° NNW |
| 5 mins | 2026-06-21 18:06:43.406Z | 54.559° ENE | 2026-06-21 18:08:43.406Z | 107.248° ESE | 27.228° | 2026-06-21 18:11:43.406Z | 159.222° S |
| 4 mins | 2026-06-21 19:41:43.406Z | 319.646° NNW | 2026-06-21 19:42:43.406Z | 301.498° NW | 17.588° | 2026-06-21 19:45:43.406Z | 250.399° W |
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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