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 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: 7 hours ago
TLE from 7 hours ago
0 ICEYE-X63
1 67372U 26004K 26095.26590261 .00003428 00000-0 37794-3 0 9990
2 67372 97.8006 95.0562 0004821 30.1644 329.9850 14.88155077 12451Epoch: 2026-04-05T06:22Z
TLE epoch observation values (Epoch: 2026-04-05T06:22:53.985Z)
Latitude
0.00003°
Longitude
165.75746°
Altitude
603.821 km
Speed
7.559 km/s
True Right ascension
06h 20m 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
19:17:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
604.09 km
Perigee altitude
597.361 km
Semi-major axis
6,978.863 km
Eccentricity
0.00048
Inclination
97.8006°
RAAN
95.0562°
Arg. of periapsis
30.1644°
True anomaly
329.95735°
Mean anomaly
329.985°
Eccentric anomaly
329.97118°
Mean motion
3.72277 °/min
Orbital period
96.7 mins
BSTAR
0.00037794
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-05 13:23:54.355Z | 351.08° N | 2026-04-05 13:26:54.355Z | 298.655° NW | 29.876° | 2026-04-05 13:30:54.355Z | 223.567° SW |
| 6 mins | 2026-04-06 00:15:54.355Z | 188.49° SSW | 2026-04-06 00:18:54.355Z | 279.211° WNW | 38.4° | 2026-04-06 00:21:54.355Z | 334.988° NNW |
| 5 mins | 2026-04-06 12:01:54.355Z | 60.343° ENE | 2026-04-06 12:03:54.355Z | 101.728° ESE | 22.264° | 2026-04-06 12:06:54.355Z | 148.994° SSE |
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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