ICEYE-X63, 67372
Orbit data source: Space-Track
ICEYE-X63, 67372 is a Finnish payload satellite 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: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X63
1 67372U 26004K 26264.55481468 .00000504 00000-0 60171-4 0 9996
2 67372 97.8076 261.7297 0004642 153.1620 206.9838 14.88443713 37630Epoch: 2026-09-21T13:18Z
TLE epoch observation values (Epoch: 2026-09-21T13:18:55.988Z)
Latitude
0.00001°
Longitude
61.56345°
Altitude
608.722 km
Speed
7.553 km/s
True Right ascension
17h 26m 55s
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
12:35:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
603.062 km
Perigee altitude
596.584 km
Semi-major axis
6,977.96 km
Eccentricity
0.00046
Inclination
97.8076°
RAAN
261.7297°
Arg. of periapsis
153.162°
True anomaly
206.95968°
Mean anomaly
206.9838°
Eccentric anomaly
206.97174°
Mean motion
3.72349 °/min
Orbital period
96.68 mins
BSTAR
0.000060171
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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 | 2026-09-21 23:08:18.182Z | 120.677° SE | 2026-09-21 23:11:18.182Z | 68.858° E | 25.713° | 2026-09-21 23:14:18.182Z | 17.395° NNE |
| 5 mins | 2026-09-22 00:45:18.182Z | 229.44° WSW | 2026-09-22 00:47:18.182Z | 272.241° WNW | 25.099° | 2026-09-22 00:50:18.182Z | 319.368° NNW |
| 6 mins | 2026-09-22 12:29:18.182Z | 30.218° NE | 2026-09-22 12:32:18.182Z | 119.714° SE | 50.195° | 2026-09-22 12:35:18.182Z | 173.975° S |
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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