ICEYE-X72, 68504
Orbit data source: Space-Track
ICEYE-X72, 68504 is a payload satellite owned by ICEYE (FI) 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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68504 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated 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: 2 days ago
TLE from 2 days ago
0 ICEYE-X72
1 68504U 26067CS 26171.19187757 .00095480 00000-0 91467-2 0 9991
2 68504 97.7631 129.4467 0001594 63.5299 296.6084 14.92665380 12174Epoch: 2026-06-20T04:36Z
TLE epoch observation values (Epoch: 2026-06-20T04:36:18.222Z)
Latitude
0.00004°
Longitude
151.96073°
Altitude
592.174 km
Speed
7.564 km/s
True Right ascension
08h 37m 47s
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
10:53:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
587.757 km
Perigee altitude
585.536 km
Semi-major axis
6,964.783 km
Eccentricity
0.00016
Inclination
97.7631°
RAAN
129.4467°
Arg. of periapsis
63.5299°
True anomaly
296.59207°
Mean anomaly
296.6084°
Eccentric anomaly
296.60023°
Mean motion
3.73406 °/min
Orbital period
96.41 mins
BSTAR
0.0091467
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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-X72 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 | 2026-06-22 10:15:19.068Z | 7.082° NNE | 2026-06-22 10:18:19.068Z | 327.251° NNW | 42.621° | 2026-06-22 10:22:19.068Z | 200.91° SSW |
| 6 mins | 2026-06-22 21:05:19.068Z | 152.989° SSE | 2026-06-22 21:07:19.068Z | 118.37° SE | 40.885° | 2026-06-22 21:11:19.068Z | 354.411° 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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