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 spacecraft
Bus & Motor
ICEYE, Unknown motor
Mass
120 kg wet, 120 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 2.4 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 ICEYE-X64
1 67373U 26004L 26095.55727094 .00003634 00000-0 40413-3 0 9990
2 67373 97.8022 95.3052 0006681 29.5648 330.5945 14.87757757 12498Epoch: 2026-04-05T13:22Z
TLE epoch observation values (Epoch: 2026-04-05T13:22:28.209Z)
Latitude
-0.00001°
Longitude
60.82668°
Altitude
603.914 km
Speed
7.56 km/s
True Right ascension
06h 21m 13s
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
01:00:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
606.633 km
Perigee altitude
597.306 km
Semi-major axis
6,980.106 km
Eccentricity
0.00067
Inclination
97.8022°
RAAN
95.3052°
Arg. of periapsis
29.5648°
True anomaly
330.55688°
Mean anomaly
330.5945°
Eccentric anomaly
330.57569°
Mean motion
3.72178 °/min
Orbital period
96.73 mins
BSTAR
0.00040413
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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 | 2026-04-05 23:11:44.167Z | 125.872° SE | 2026-04-05 23:14:44.167Z | 77.533° E | 24.517° | 2026-04-05 23:17:44.167Z | 19.115° NNE |
| 5 mins | 2026-04-06 00:48:44.167Z | 225.636° WSW | 2026-04-06 00:50:44.167Z | 263.219° W | 21.417° | 2026-04-06 00:53:44.167Z | 314.27° NW |
| 6 mins | 2026-04-06 12:33:44.167Z | 29.865° NE | 2026-04-06 12:35:44.167Z | 80.556° E | 39.599° | 2026-04-06 12:39:44.167Z | 178.546° 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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