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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Edit Public Description
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: 9 hours ago
TLE from 9 hours ago
0 ICEYE-X45
1 62705U 25009DA 25286.65013170 .00008258 00000-0 65320-3 0 9994
2 62705 97.7776 7.3345 0001215 68.3656 291.7697 15.00888836 40709Epoch: 2025-10-13T15:36Z
TLE epoch observation values (Epoch: 2025-10-13T15:36:11.378Z)
Latitude
-0.00005°
Longitude
110.83723°
Altitude
566.895 km
Speed
7.578 km/s
True Right ascension
00h 29m 20s
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
18:49:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.005 km
Perigee altitude
560.319 km
Semi-major axis
6,939.299 km
Eccentricity
0.00012
Inclination
97.7776°
RAAN
7.3345°
Arg. of periapsis
68.3656°
True anomaly
291.75677°
Mean anomaly
291.7697°
Eccentric anomaly
291.76323°
Mean motion
3.75465 °/min
Orbital period
95.88 mins
BSTAR
0.0006532
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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 | 2025-10-14 04:33:29.491Z | 107.386° ESE | 2025-10-14 04:35:29.491Z | 74.595° E | 17.743° | 2025-10-14 04:38:29.491Z | 24.222° NE |
| 5 mins | 2025-10-14 06:08:29.491Z | 213.388° SW | 2025-10-14 06:10:29.491Z | 259.076° W | 27.361° | 2025-10-14 06:13:29.491Z | 320.837° NNW |
| 5 mins | 2025-10-14 17:47:29.491Z | 45.79° ENE | 2025-10-14 17:49:29.491Z | 89.077° E | 27.349° | 2025-10-14 17:52:29.491Z | 154.08° 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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