ICEYE-X64, 67373
Orbit data source: Space-Track
ICEYE-X64, 67373 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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67373 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated business
Manufacturer
ICEYE
Mission
Operational Defense 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
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ICEYE-X64
1 67373U 26004L 26146.26708508 .00001293 00000-0 14731-3 0 9997
2 67373 97.8015 145.1912 0005314 193.2986 166.8091 14.87859183 20032Epoch: 2026-05-26T06:24Z
TLE epoch observation values (Epoch: 2026-05-26T06:24:36.150Z)
Latitude
-0.00008°
Longitude
165.19761°
Altitude
611.275 km
Speed
7.552 km/s
True Right ascension
09h 40m 45s
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
03:37:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.361 km
Perigee altitude
597.943 km
Semi-major axis
6,979.789 km
Eccentricity
0.00053
Inclination
97.8015°
RAAN
145.1912°
Arg. of periapsis
193.2986°
True anomaly
166.82299°
Mean anomaly
166.8091°
Eccentric anomaly
166.81604°
Mean motion
3.72203 °/min
Orbital period
96.72 mins
BSTAR
0.00014731
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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-X64 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 | 2026-05-27 00:18:22.776Z | 196.339° SSW | 2026-05-27 00:20:22.776Z | 253.891° W | 37.687° | 2026-05-27 00:24:22.776Z | 335.941° NNW |
| 5 mins | 2026-05-27 12:03:22.776Z | 50.5° ENE | 2026-05-27 12:05:22.776Z | 87.682° E | 23.337° | 2026-05-27 12:08:22.776Z | 144.981° SSE |
| 5 mins | 2026-05-27 13:39:22.776Z | 331.092° NNW | 2026-05-27 13:41:22.776Z | 291.959° WNW | 22.762° | 2026-05-27 13:44:22.776Z | 240.34° 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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