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: 2 days ago
TLE from 2 days ago
0 ICEYE-X75
1 68497U 26067CK 26258.62781703 .00001044 00000-0 10776-3 0 9995
2 68497 97.7691 215.6004 0002387 47.8676 312.2746 14.92280322 25219Epoch: 2026-09-15T15:04Z
TLE epoch observation values (Epoch: 2026-09-15T15:04:03.391Z)
Latitude
0.00003°
Longitude
-5.00477°
Altitude
592.75 km
Speed
7.564 km/s
True Right ascension
14h 22m 24s
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
05:14:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
589.509 km
Perigee altitude
586.183 km
Semi-major axis
6,965.983 km
Eccentricity
0.00024
Inclination
97.7691°
RAAN
215.6004°
Arg. of periapsis
47.8676°
True anomaly
312.25436°
Mean anomaly
312.2746°
Eccentric anomaly
312.26448°
Mean motion
3.7331 °/min
Orbital period
96.43 mins
BSTAR
0.00010776
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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 | 2026-09-17 20:19:02.791Z | 115.273° SE | 2026-09-17 20:22:02.791Z | 67.824° E | 20.726° | 2026-09-17 20:25:02.791Z | 20.374° NNE |
| 6 mins | 2026-09-17 21:55:02.791Z | 212.773° SW | 2026-09-17 21:57:02.791Z | 253.477° W | 30.319° | 2026-09-17 22:01:02.791Z | 325.873° NNW |
| 6 mins | 2026-09-18 09:38:02.791Z | 38.695° NE | 2026-09-18 09:41:02.791Z | 115.657° SE | 37.518° | 2026-09-18 09:44:02.791Z | 165.517° 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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