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 26023.44028460 .00010603 00000-0 63321-3 0 9991
2 62384 44.9983 49.2804 0002893 294.5419 65.5156 15.11299203 60260Epoch: 2026-01-23T10:34Z
TLE epoch observation values (Epoch: 2026-01-23T10:34:00.589Z)
Latitude
-0.00002°
Longitude
127.99886°
Altitude
531.407 km
Speed
7.599 km/s
True Right ascension
03h 17m 07s
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
04:06:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
535.835 km
Perigee altitude
531.835 km
Semi-major axis
6,911.972 km
Eccentricity
0.00029
Inclination
44.9983°
RAAN
49.2804°
Arg. of periapsis
294.5419°
True anomaly
65.54577°
Mean anomaly
65.5156°
Eccentric anomaly
65.53069°
Mean motion
3.77694 °/min
Orbital period
95.32 mins
BSTAR
0.00063321
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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 | 2026-01-24 04:12:05.184Z | 195.642° SSW | 2026-01-24 04:15:05.184Z | 133.296° SE | 24.874° | 2026-01-24 04:18:05.184Z | 84.639° E |
| 6 mins | 2026-01-24 05:52:05.184Z | 259.493° W | 2026-01-24 05:54:05.184Z | 302.658° NW | 42.532° | 2026-01-24 05:58:05.184Z | 63.851° ENE |
| 6 mins | 2026-01-24 07:32:05.184Z | 296.403° NW | 2026-01-24 07:35:05.184Z | 14.635° NNE | 31.638° | 2026-01-24 07:38:05.184Z | 66.492° ENE |
| 6 mins | 2026-01-24 09:12:05.184Z | 300.535° NW | 2026-01-24 09:15:05.184Z | 24.189° NE | 40.445° | 2026-01-24 09:18:05.184Z | 94.269° ESE |
| 6 mins | 2026-01-24 10:52:05.184Z | 275.099° WNW | 2026-01-24 10:55:05.184Z | 203.136° SW | 31.265° | 2026-01-24 10:58:05.184Z | 148.177° 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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