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: 22 hours ago
TLE from 22 hours ago
0 ICEYE-X45
1 62705U 25009DA 25334.78563398 .00002740 00000-0 22017-3 0 9990
2 62705 97.7904 55.5443 0001680 84.5367 275.6048 15.00867297 47921Epoch: 2025-11-30T18:51Z
TLE epoch observation values (Epoch: 2025-11-30T18:51:18.775Z)
Latitude
-0.00007°
Longitude
62.82158°
Altitude
567.16 km
Speed
7.578 km/s
True Right ascension
03h 42m 10s
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
15:01:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.395 km
Perigee altitude
560.063 km
Semi-major axis
6,939.366 km
Eccentricity
0.00017
Inclination
97.7904°
RAAN
55.5443°
Arg. of periapsis
84.5367°
True anomaly
275.58564°
Mean anomaly
275.6048°
Eccentric anomaly
275.59522°
Mean motion
3.7546 °/min
Orbital period
95.88 mins
BSTAR
0.00022017
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-01 17:49:38.289Z | 35.786° NE | 2025-12-01 17:52:38.289Z | 89.249° E | 27.37° | 2025-12-01 17:55:38.289Z | 154.186° SSE |
| 4 mins | 2025-12-02 04:37:38.289Z | 93.802° ESE | 2025-12-02 04:38:38.289Z | 75.392° E | 17.742° | 2025-12-02 04:41:38.289Z | 24.596° NE |
| 5 mins | 2025-12-02 06:11:38.289Z | 212.92° SW | 2025-12-02 06:13:38.289Z | 257.833° W | 27.266° | 2025-12-02 06:16:38.289Z | 320.377° NNW |
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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