ICEYE-X47, 62389
Orbit data source: Space-Track
ICEYE-X47, 62389 is a payload satellite owned by ICEYE (FI) in LEO that was launched on Sat, 21 Dec 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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62389 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
FI / FINRelated 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: 1 day ago
TLE from 1 day ago
0 ICEYE-X47
1 62389U 24247N 25300.02209765 .00007405 00000-0 46630-3 0 9996
2 62389 44.9955 159.4652 0001622 130.0405 230.0614 15.09739917 46896Epoch: 2025-10-27T00:31Z
TLE epoch observation values (Epoch: 2025-10-27T00:31:49.236Z)
Latitude
-0.00001°
Longitude
115.88013°
Altitude
537.712 km
Speed
7.595 km/s
True Right ascension
10h 37m 51s
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
03:53:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.713 km
Perigee altitude
537.47 km
Semi-major axis
6,916.729 km
Eccentricity
0.00016
Inclination
44.9955°
RAAN
159.4652°
Arg. of periapsis
130.0405°
True anomaly
230.04715°
Mean anomaly
230.0614°
Eccentric anomaly
230.05428°
Mean motion
3.77305 °/min
Orbital period
95.41 mins
BSTAR
0.0004663
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Other satellites on launch #247 in the year 2024 (2024-12-21 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-X47 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-28 16:23:55.509Z | 174.382° S | 2025-10-28 16:25:55.509Z | 143.356° SSE | 15.56° | 2025-10-28 16:27:55.509Z | 109.587° ESE |
| 6 mins | 2025-10-28 18:02:55.509Z | 237.752° WSW | 2025-10-28 18:05:55.509Z | 118.283° SE | 43.944° | 2025-10-28 18:08:55.509Z | 69.161° E |
| 5 mins | 2025-10-28 19:43:55.509Z | 293.421° NW | 2025-10-28 19:45:55.509Z | 351.034° N | 34.31° | 2025-10-28 19:48:55.509Z | 59.463° ENE |
| 6 mins | 2025-10-28 21:23:55.509Z | 304.967° NW | 2025-10-28 21:25:55.509Z | 347.364° N | 34.415° | 2025-10-28 21:29:55.509Z | 83.335° E |
| 6 mins | 2025-10-28 23:03:55.509Z | 285.595° WNW | 2025-10-28 23:06:55.509Z | 176.403° S | 41.01° | 2025-10-28 23:09:55.509Z | 128.595° SE |
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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