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 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, 14.5 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X74
1 68500U 26067CN 26150.88770204 .00003624 00000-0 36684-3 0 9995
2 68500 97.7607 109.3990 0003845 82.6107 277.5548 14.91575161 9144Epoch: 2026-05-30T21:18Z
TLE epoch observation values (Epoch: 2026-05-30T21:18:17.456Z)
Latitude
-0.00006°
Longitude
-98.571°
Altitude
595.713 km
Speed
7.562 km/s
True Right ascension
07h 17m 35s
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
21:34:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
592.722 km
Perigee altitude
587.363 km
Semi-major axis
6,968.18 km
Eccentricity
0.00038
Inclination
97.7607°
RAAN
109.399°
Arg. of periapsis
82.6107°
True anomaly
277.51112°
Mean anomaly
277.5548°
Eccentric anomaly
277.53296°
Mean motion
3.73133 °/min
Orbital period
96.48 mins
BSTAR
0.00036684
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-31 21:35:10.454Z | 189.329° SSW | 2026-05-31 21:38:10.454Z | 275.193° WNW | 37.833° | 2026-05-31 21:41:10.454Z | 334.052° NNW |
| 5 mins | 2026-06-01 09:19:10.454Z | 53.757° ENE | 2026-06-01 09:21:10.454Z | 91.331° ESE | 21.839° | 2026-06-01 09:24:10.454Z | 144.572° SSE |
| 5 mins | 2026-06-01 10:55:10.454Z | 326.961° NNW | 2026-06-01 10:57:10.454Z | 282.572° WNW | 23.616° | 2026-06-01 11:00:10.454Z | 234.914° WSW |
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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