ICEYE-X75, 68497
Orbit data source: Space-Track
ICEYE-X75, 68497 is a payload satellite owned by ICEYE (PL) 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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68497 intel report (Beta)
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Identifier
Orbit
Country
PL / POLRelated 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, 0.7 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 ICEYE-X75
1 68497U 26067CK 26171.38758391 .00000758 00000-0 80055-4 0 9998
2 68497 97.7591 129.6172 0000793 22.7558 337.3696 14.92126529 12203Epoch: 2026-06-20T09:18Z
TLE epoch observation values (Epoch: 2026-06-20T09:18:07.249Z)
Latitude
-0.00004°
Longitude
81.48407°
Altitude
593.838 km
Speed
7.563 km/s
True Right ascension
08h 38m 28s
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
07:17:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.877 km
Perigee altitude
587.772 km
Semi-major axis
6,966.461 km
Eccentricity
0.00008
Inclination
97.7591°
RAAN
129.6172°
Arg. of periapsis
22.7558°
True anomaly
337.3661°
Mean anomaly
337.3696°
Eccentric anomaly
337.36785°
Mean motion
3.73271 °/min
Orbital period
96.44 mins
BSTAR
0.000080055
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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-X75 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 | 2026-06-20 20:42:16.283Z | 133.476° SE | 2026-06-20 20:45:16.283Z | 73.887° E | 30.588° | 2026-06-20 20:48:16.283Z | 10.943° NNE |
| 6 mins | 2026-06-21 10:01:16.283Z | 18.025° NNE | 2026-06-21 10:04:16.283Z | 128.487° SE | 43.883° | 2026-06-21 10:07:16.283Z | 186.586° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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