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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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, 2.4 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X49
1 62384U 24247H 26171.20594928 .00003640 00000-0 21689-3 0 9990
2 62384 44.9994 341.2782 0001216 265.2379 94.8359 15.13006360 82637Epoch: 2026-06-20T04:56Z
TLE epoch observation values (Epoch: 2026-06-20T04:56:34.017Z)
Latitude
-0.00007°
Longitude
-1.28751°
Altitude
527.107 km
Speed
7.601 km/s
True Right ascension
22h 45m 06s
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
07:18:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
529.477 km
Perigee altitude
527.797 km
Semi-major axis
6,906.774 km
Eccentricity
0.00012
Inclination
44.9994°
RAAN
341.2782°
Arg. of periapsis
265.2379°
True anomaly
94.84978°
Mean anomaly
94.8359°
Eccentric anomaly
94.84284°
Mean motion
3.78121 °/min
Orbital period
95.21 mins
BSTAR
0.00021689
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 21:18:46.734Z | 268.504° W | 2026-06-20 21:21:46.734Z | 216.837° SW | 20.799° | 2026-06-20 21:24:46.734Z | 167.282° S |
| 5 mins | 2026-06-21 14:26:46.734Z | 218.668° SW | 2026-06-21 14:28:46.734Z | 149.36° SSE | 39.885° | 2026-06-21 14:31:46.734Z | 75.143° E |
| 6 mins | 2026-06-21 16:05:46.734Z | 277.637° WNW | 2026-06-21 16:08:46.734Z | 355.64° N | 36.363° | 2026-06-21 16:11:46.734Z | 59.732° ENE |
| 5 mins | 2026-06-21 17:46:46.734Z | 308.361° NW | 2026-06-21 17:48:46.734Z | 2.195° NNE | 33.329° | 2026-06-21 17:51:46.734Z | 72.873° E |
| 6 mins | 2026-06-21 19:26:46.734Z | 292.214° WNW | 2026-06-21 19:28:46.734Z | 263.302° W | 44.754° | 2026-06-21 19:32:46.734Z | 116.598° SE |
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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