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: 11 hours ago
TLE from 11 hours ago
0 ICEYE-X49
1 62384U 24247H 26282.88542417 .00003483 00000-0 20491-3 0 9998
2 62384 44.9968 104.6419 0001274 268.9618 91.1114 15.13584330 99552Epoch: 2026-10-09T21:15Z
TLE epoch observation values (Epoch: 2026-10-09T21:15:00.648Z)
Latitude
0.00002°
Longitude
127.38873°
Altitude
525.295 km
Speed
7.602 km/s
True Right ascension
06h 58m 34s
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
02:52:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
527.759 km
Perigee altitude
526 km
Semi-major axis
6,905.017 km
Eccentricity
0.00013
Inclination
44.9968°
RAAN
104.6419°
Arg. of periapsis
268.9618°
True anomaly
91.126°
Mean anomaly
91.1114°
Eccentric anomaly
91.1187°
Mean motion
3.78265 °/min
Orbital period
95.17 mins
BSTAR
0.00020491
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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 | 2026-10-10 14:51:20.312Z | 198.193° SSW | 2026-10-10 14:54:20.312Z | 138.055° SSE | 28.465° | 2026-10-10 14:57:20.312Z | 85.495° E |
| 6 mins | 2026-10-10 16:31:20.312Z | 260.325° W | 2026-10-10 16:33:20.312Z | 302.685° NW | 64.648° | 2026-10-10 16:37:20.312Z | 63.388° ENE |
| 6 mins | 2026-10-10 18:11:20.312Z | 298.131° NW | 2026-10-10 18:13:20.312Z | 340.595° N | 37.189° | 2026-10-10 18:17:20.312Z | 67.033° ENE |
| 6 mins | 2026-10-10 19:51:20.312Z | 302.403° NW | 2026-10-10 19:54:20.312Z | 43.245° NE | 55.057° | 2026-10-10 19:57:20.312Z | 95.226° ESE |
| 6 mins | 2026-10-10 21:31:20.312Z | 271.098° WNW | 2026-10-10 21:33:20.312Z | 225.039° WSW | 37.36° | 2026-10-10 21:37:20.312Z | 145.483° 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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