ICEYE-X64, 67373
Orbit data source: Space-Track
ICEYE-X64, 67373 is a payload satellite owned by RNAF (NL) 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
NL / NETHRelated 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ICEYE-X64
1 67373U 26004L 26264.35118878 .00000490 00000-0 59164-4 0 9991
2 67373 97.8089 261.4211 0006123 165.5118 194.6275 14.88079394 37596Epoch: 2026-09-21T08:25Z
TLE epoch observation values (Epoch: 2026-09-21T08:25:42.710Z)
Latitude
-0.00005°
Longitude
134.76088°
Altitude
611.11 km
Speed
7.551 km/s
True Right ascension
17h 25m 41s
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
12:36:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
605.236 km
Perigee altitude
596.69 km
Semi-major axis
6,979.1 km
Eccentricity
0.00061
Inclination
97.8089°
RAAN
261.4211°
Arg. of periapsis
165.5118°
True anomaly
194.60979°
Mean anomaly
194.6275°
Eccentric anomaly
194.61865°
Mean motion
3.72258 °/min
Orbital period
96.71 mins
BSTAR
0.000059164
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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 | 2026-09-21 23:05:58.813Z | 116.928° SE | 2026-09-21 23:08:58.813Z | 63.355° ENE | 24.443° | 2026-09-21 23:11:58.813Z | 16.199° NNE |
| 6 mins | 2026-09-22 00:41:58.813Z | 216.923° SW | 2026-09-22 00:43:58.813Z | 253.234° W | 26.276° | 2026-09-22 00:47:58.813Z | 322.105° NNW |
| 6 mins | 2026-09-22 12:26:58.813Z | 32.153° NE | 2026-09-22 12:29:58.813Z | 120.036° SE | 47.271° | 2026-09-22 12:32:58.813Z | 172.416° 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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