ICEYE-X63, 67372
Orbit data source: Space-Track
ICEYE-X63, 67372 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Sun, 11 Jan 2026 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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67372 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
120 kg wet, 120 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: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X63
1 67372U 26004K 26206.40320435 .00001005 00000-0 11445-3 0 9998
2 67372 97.8021 204.4491 0004709 24.5063 335.6376 14.88364682 28988Epoch: 2026-07-25T09:40Z
TLE epoch observation values (Epoch: 2026-07-25T09:40:36.855Z)
Latitude
-0.00012°
Longitude
116.17957°
Altitude
603.085 km
Speed
7.56 km/s
True Right ascension
13h 37m 47s
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
11:10:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
603.356 km
Perigee altitude
596.784 km
Semi-major axis
6,978.207 km
Eccentricity
0.00047
Inclination
97.8021°
RAAN
204.4491°
Arg. of periapsis
24.5063°
True anomaly
335.61533°
Mean anomaly
335.6376°
Eccentric anomaly
335.62647°
Mean motion
3.72329 °/min
Orbital period
96.69 mins
BSTAR
0.00011445
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Other satellites on launch #4 in the year 2026 (2026-01-11 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-X63 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 | 2026-07-26 00:19:48.830Z | 193.438° SSW | 2026-07-26 00:22:48.830Z | 276.447° WNW | 35.916° | 2026-07-26 00:25:48.830Z | 332.164° NNW |
| 5 mins | 2026-07-26 12:05:48.830Z | 59.793° ENE | 2026-07-26 12:07:48.830Z | 105.062° ESE | 24.242° | 2026-07-26 12:10:48.830Z | 152.936° SSE |
| 5 mins | 2026-07-26 13:40:48.830Z | 333.745° NNW | 2026-07-26 13:42:48.830Z | 297.959° NW | 21.909° | 2026-07-26 13:45:48.830Z | 244.152° WSW |
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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