ICEYE-X49, 62384
Orbit data source: Space-Track
ICEYE-X49, 62384 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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62384 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: 16 hours ago
TLE from 16 hours ago
0 ICEYE-X49
1 62384U 24247H 26036.52672732 .00015561 00000-0 91406-3 0 9994
2 62384 45.0000 339.5879 0001346 339.4871 20.5952 15.11605953 62240Epoch: 2026-02-05T12:38Z
TLE epoch observation values (Epoch: 2026-02-05T12:38:29.240Z)
Latitude
0.00001°
Longitude
14.28839°
Altitude
530.43 km
Speed
7.6 km/s
True Right ascension
22h 38m 21s
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
06:38:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
533.83 km
Perigee altitude
531.97 km
Semi-major axis
6,911.037 km
Eccentricity
0.00013
Inclination
45°
RAAN
339.5879°
Arg. of periapsis
339.4871°
True anomaly
20.60063°
Mean anomaly
20.5952°
Eccentric anomaly
20.59791°
Mean motion
3.77771 °/min
Orbital period
95.3 mins
BSTAR
0.00091406
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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-X49 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-02-06 04:58:43.474Z | 286.507° WNW | 2026-02-06 05:01:43.474Z | 217.191° SW | 41.153° | 2026-02-06 05:05:43.474Z | 128.944° SE |
| 4 mins | 2026-02-06 22:08:43.474Z | 164.96° S | 2026-02-06 22:09:43.474Z | 144.379° SSE | 19.791° | 2026-02-06 22:12:43.474Z | 93.14° ESE |
| 6 mins | 2026-02-06 23:46:43.474Z | 247.864° W | 2026-02-06 23:49:43.474Z | 51.773° ENE | 44.026° | 2026-02-06 23:52:43.474Z | 65.715° ENE |
| 5 mins | 2026-02-07 01:27:43.474Z | 300.81° NW | 2026-02-07 01:29:43.474Z | 0.985° NNE | 32.855° | 2026-02-07 01:32:43.474Z | 62.161° ENE |
| 6 mins | 2026-02-07 03:07:43.474Z | 307.325° NW | 2026-02-07 03:09:43.474Z | 2.786° NNE | 37.482° | 2026-02-07 03:13:43.474Z | 90.262° ESE |
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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