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: 18 hours ago
TLE from 18 hours ago
0 ICEYE-X75
1 68497U 26067CK 26283.63824165 .00001173 00000-0 12029-3 0 9990
2 68497 97.7740 240.2796 0000489 10.3885 349.7344 14.92321585 28943Epoch: 2026-10-10T15:19Z
TLE epoch observation values (Epoch: 2026-10-10T15:19:04.078Z)
Latitude
-0.00003°
Longitude
-8.72989°
Altitude
593.405 km
Speed
7.563 km/s
True Right ascension
16h 01m 07s
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
03:34:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
588.058 km
Perigee altitude
587.377 km
Semi-major axis
6,965.855 km
Eccentricity
0.00005
Inclination
97.774°
RAAN
240.2796°
Arg. of periapsis
10.3885°
True anomaly
349.7334°
Mean anomaly
349.7344°
Eccentric anomaly
349.7339°
Mean motion
3.7332 °/min
Orbital period
96.43 mins
BSTAR
0.00012029
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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 | 2026-10-11 09:35:46.792Z | 34.52° NE | 2026-10-11 09:38:46.792Z | 93.802° ESE | 37.049° | 2026-10-11 09:41:46.792Z | 159.507° S |
| 4 mins | 2026-10-11 11:12:46.792Z | 317.045° NNW | 2026-10-11 11:13:46.792Z | 299.92° NW | 17.493° | 2026-10-11 11:16:46.792Z | 252.77° W |
| 5 mins | 2026-10-11 20:26:46.792Z | 104.682° ESE | 2026-10-11 20:28:46.792Z | 63.596° ENE | 24.009° | 2026-10-11 20:31:46.792Z | 16.131° NNE |
| 5 mins | 2026-10-11 22:01:46.792Z | 220.119° SW | 2026-10-11 22:03:46.792Z | 259.476° W | 26.05° | 2026-10-11 22:06:46.792Z | 315.544° NNW |
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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