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 Commercial 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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X75
1 68497U 26067CK 26217.45634961 .00000646 00000-0 68836-4 0 9992
2 68497 97.7625 175.0067 0002742 113.5603 246.5904 14.92215916 19079Epoch: 2026-08-05T10:57Z
TLE epoch observation values (Epoch: 2026-08-05T10:57:08.606Z)
Latitude
-0.00003°
Longitude
56.71036°
Altitude
594.83 km
Speed
7.562 km/s
True Right ascension
11h 40m 01s
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
16:18:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.956 km
Perigee altitude
586.136 km
Semi-major axis
6,966.183 km
Eccentricity
0.00027
Inclination
97.7625°
RAAN
175.0067°
Arg. of periapsis
113.5603°
True anomaly
246.56157°
Mean anomaly
246.5904°
Eccentric anomaly
246.57598°
Mean motion
3.73294 °/min
Orbital period
96.44 mins
BSTAR
0.000068836
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-06 10:02:50.953Z | 14.973° NNE | 2026-08-06 10:06:50.953Z | 165.142° S | 43.31° | 2026-08-06 10:09:50.953Z | 189.409° SSW |
| 6 mins | 2026-08-06 20:53:50.953Z | 135.949° SSE | 2026-08-06 20:55:50.953Z | 81.01° E | 36.646° | 2026-08-06 20:59:50.953Z | 359.829° N |
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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