ICEYE-X74, 68500
Orbit data source: Space-Track
ICEYE-X74, 68500 is a payload satellite owned by ICEYE (US) 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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68500 intel report (Beta)
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Identifier
Orbit
Country
USRelated 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, 0.8 m
Radar Cross Section
0.776 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 ICEYE-X74
1 68500U 26067CN 26258.13712273 .00001587 00000-0 16147-3 0 9992
2 68500 97.7714 215.0666 0003901 82.3208 277.8454 14.92160480 25131Epoch: 2026-09-15T03:17Z
TLE epoch observation values (Epoch: 2026-09-15T03:17:27.403Z)
Latitude
-0.00003°
Longitude
171.59504°
Altitude
593.872 km
Speed
7.563 km/s
True Right ascension
14h 20m 15s
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
06:24:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
590.937 km
Perigee altitude
585.502 km
Semi-major axis
6,966.356 km
Eccentricity
0.00039
Inclination
97.7714°
RAAN
215.0666°
Arg. of periapsis
82.3208°
True anomaly
277.80111°
Mean anomaly
277.8454°
Eccentric anomaly
277.82326°
Mean motion
3.7328 °/min
Orbital period
96.44 mins
BSTAR
0.00016147
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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-X74 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 | 2026-09-16 21:15:27.058Z | 167.121° S | 2026-09-16 21:18:27.058Z | 171.372° S | 71.797° | 2026-09-16 21:22:27.058Z | 347.212° N |
| 6 mins | 2026-09-17 10:35:27.058Z | 345.949° N | 2026-09-17 10:37:27.058Z | 296.987° NW | 41.946° | 2026-09-17 10:41:27.058Z | 217.309° SW |
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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