ICEYE-X62, 66755
Orbit data source: Space-Track
ICEYE-X62, 66755 is a payload satellite owned by ICEYE (PL) 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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66755 intel report (Beta)
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Identifier
Orbit
Country
PL / POLRelated 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: 13 hours ago
TLE from 13 hours ago
0 ICEYE-X62
1 66755U 25276CT 26238.16455350 .00001884 00000-0 11856-3 0 9996
2 66755 97.4155 308.1770 0003999 112.5164 247.6490 15.10367883 40893Epoch: 2026-08-26T03:56Z
TLE epoch observation values (Epoch: 2026-08-26T03:56:57.422Z)
Latitude
0.00003°
Longitude
-85.48374°
Altitude
539.207 km
Speed
7.592 km/s
True Right ascension
20h 32m 42s
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
08:23:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.82 km
Perigee altitude
529.293 km
Semi-major axis
6,910.193 km
Eccentricity
0.0004
Inclination
97.4155°
RAAN
308.177°
Arg. of periapsis
112.5164°
True anomaly
247.60663°
Mean anomaly
247.649°
Eccentric anomaly
247.62781°
Mean motion
3.7784 °/min
Orbital period
95.28 mins
BSTAR
0.00011856
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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-X62 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 | 2026-08-26 17:14:01.957Z | 27.177° NE | 2026-08-26 17:17:01.957Z | 83.348° E | 34.319° | 2026-08-26 17:20:01.957Z | 166.261° S |
| 4 mins | 2026-08-27 03:58:01.957Z | 97.522° ESE | 2026-08-27 03:59:01.957Z | 76.971° E | 19.546° | 2026-08-27 04:02:01.957Z | 22.176° NNE |
| 4 mins | 2026-08-27 05:32:01.957Z | 226.649° WSW | 2026-08-27 05:34:01.957Z | 273.552° WNW | 22.686° | 2026-08-27 05:36:01.957Z | 312.224° NW |
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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