ICEYE-X72, 68504
Orbit data source: Space-Track
ICEYE-X72, 68504 is a payload satellite owned by ICEYE (FI) in SSO that was launched on Mon, 30 Mar 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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68504 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, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 ICEYE-X72
1 68504U 26067CS 26154.42715127 .00003769 00000-0 37673-3 0 9995
2 68504 97.7627 112.9239 0003052 55.0567 305.0938 14.92055464 9678Epoch: 2026-06-03T10:15Z
TLE epoch observation values (Epoch: 2026-06-03T10:15:05.869Z)
Latitude
-0.00007°
Longitude
67.26353°
Altitude
593.347 km
Speed
7.564 km/s
True Right ascension
07h 31m 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
03:10:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.672 km
Perigee altitude
586.42 km
Semi-major axis
6,966.683 km
Eccentricity
0.00031
Inclination
97.7627°
RAAN
112.9239°
Arg. of periapsis
55.0567°
True anomaly
305.06518°
Mean anomaly
305.0938°
Eccentric anomaly
305.07949°
Mean motion
3.73254 °/min
Orbital period
96.45 mins
BSTAR
0.00037673
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Other satellites on launch #67 in the year 2026 (2026-03-30 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-X72 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 | 2026-06-06 20:28:26.149Z | 123.811° SE | 2026-06-06 20:31:26.149Z | 74.658° E | 23.395° | 2026-06-06 20:34:26.149Z | 18.953° NNE |
| 5 mins | 2026-06-06 22:05:26.149Z | 229.922° WSW | 2026-06-06 22:07:26.149Z | 271.965° WNW | 21.923° | 2026-06-06 22:10:26.149Z | 318.957° NNW |
| 6 mins | 2026-06-07 09:47:26.149Z | 28.667° NE | 2026-06-07 09:50:26.149Z | 105.412° ESE | 37.7° | 2026-06-07 09:53:26.149Z | 172.097° 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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