ICEYE-X61, 66754
Orbit data source: Space-Track
ICEYE-X61, 66754 is a Finnish payload satellite in SSO that was launched on Fri, 28 Nov 2025 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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66754 intel report (Beta)
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Identifier
Orbit
Country
FI / FINRelated business
None
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: 15 hours ago
TLE from 15 hours ago
0 ICEYE-X61
1 66754U 25276CS 26238.66206234 .00003315 00000-0 16202-3 0 9996
2 66754 97.4159 310.8361 0004937 90.9779 269.2021 15.18914877 41111Epoch: 2026-08-26T15:53Z
TLE epoch observation values (Epoch: 2026-08-26T15:53:22.186Z)
Latitude
-0.00002°
Longitude
97.58182°
Altitude
512.256 km
Speed
7.608 km/s
True Right ascension
20h 43m 20s
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
22:33:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
509.485 km
Perigee altitude
502.688 km
Semi-major axis
6,884.224 km
Eccentricity
0.00049
Inclination
97.4159°
RAAN
310.8361°
Arg. of periapsis
90.9779°
True anomaly
269.14553°
Mean anomaly
269.2021°
Eccentric anomaly
269.17382°
Mean motion
3.7998 °/min
Orbital period
94.74 mins
BSTAR
0.00016202
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Other satellites on launch #276 in the year 2025 (2025-11-28 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-X61 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 | 2026-08-27 17:44:52.369Z | 12.811° NNE | 2026-08-27 17:47:52.369Z | 42.82° NE | 44.859° | 2026-08-27 17:50:52.369Z | 191.673° SSW |
| 4 mins | 2026-08-28 04:24:52.369Z | 113.431° SE | 2026-08-28 04:25:52.369Z | 86.462° E | 27.487° | 2026-08-28 04:28:52.369Z | 14.051° NNE |
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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