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 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: 11 hours ago
TLE from 11 hours ago
0 ICEYE-X72
1 68504U 26067CS 26263.35294098 .00001851 00000-0 15883-3 0 9996
2 68504 97.7705 221.0270 0002750 51.9458 308.2013 14.98716835 25961Epoch: 2026-09-20T08:28Z
TLE epoch observation values (Epoch: 2026-09-20T08:28:14.100Z)
Latitude
0.00003°
Longitude
94.7199°
Altitude
572.729 km
Speed
7.575 km/s
True Right ascension
14h 44m 06s
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
11:57:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
569.78 km
Perigee altitude
565.96 km
Semi-major axis
6,946.007 km
Eccentricity
0.00028
Inclination
97.7705°
RAAN
221.027°
Arg. of periapsis
51.9458°
True anomaly
308.17653°
Mean anomaly
308.2013°
Eccentric anomaly
308.18892°
Mean motion
3.74921 °/min
Orbital period
96.02 mins
BSTAR
0.00015883
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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 | 2026-09-20 21:24:14.546Z | 172.303° S | 2026-09-20 21:28:14.546Z | 293.008° NW | 72.377° | 2026-09-20 21:31:14.546Z | 342.923° N |
| 5 mins | 2026-09-21 10:41:14.546Z | 343.058° N | 2026-09-21 10:43:14.546Z | 292.672° NW | 38.795° | 2026-09-21 10:46:14.546Z | 224.891° 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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