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ICEYE-X59, 66752

Orbit data source: Space-Track

ICEYE-X59, 66752 is a Greek 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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Iframe URL

https://www.satcat.com/sats-embedded/66752?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

66752, 2025-276CQ

Orbit

SSO

Country

GR / GREC

Related business

Hellenic Space Center (GR)

Manufacturer

ICEYE

Mission

Operational Commercial Radar Imaging

Bus & Motor

ICEYE, Unknown motor

Mass

120 kg wet, 120 kg dry

Launch date (UTC)

2025-11-28 (4 months ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 1 Pan, 2.4 m

Radar Cross Section

0.776 m²

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 ICEYE-X59
1 66752U 25276CQ  26092.21625314  .00003927  00000-0  24913-3 0  9994
2 66752  97.4211 166.5795 0004272 162.2566 197.8813 15.09452468 18857

Epoch: 2026-04-02T05:11Z

TLE epoch observation values (Epoch: 2026-04-02T05:11:24.271Z)

Latitude

-0.00004°

Longitude

-101.83954°

Altitude

543.76 km

Speed

7.589 km/s

True Right ascension

11h 06m 19s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

23:23:17

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

537.806 km

Perigee altitude

531.899 km

Semi-major axis

6,912.99 km

Eccentricity

0.00043

Inclination

97.4211°

RAAN

166.5795°

Arg. of periapsis

162.2566°

True anomaly

197.86628°

Mean anomaly

197.8813°

Eccentric anomaly

197.87379°

Mean motion

3.77611 °/min

Orbital period

95.34 mins

BSTAR

0.00024913

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Other satellites on launch #276 in the year 2025 (2025-11-28 UTC)

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ICEYE-X59 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	2026-04-02 18:28:26.431Z	345.409° N	2026-04-02 18:31:26.431Z	290.915° WNW	24.036°	2026-04-02 18:34:26.431Z	234.222° WSW
6 mins	2026-04-03 05:11:26.431Z	186.034° SSW	2026-04-03 05:13:26.431Z	232.258° WSW	39.364°	2026-04-03 05:17:26.431Z	339.411° N

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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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Check out ICEYE-X59, 66752 on other resources

View ICEYE-X59, 66752 on NASA - NSSDCA Website

View ICEYE-X59, 66752 on Heavens-Above

View ICEYE-X59, 66752 on Keep Track

View ICEYE-X59, 66752 on Celestrak

View ICEYE-X59, 66752 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

ICEYE-X59, 66752

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-04-02T05:11:24.271Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #276 in the year 2025 (2025-11-28 UTC)

ICEYE-X59 Visibility forecast

Co-orbital & Co-planar RSOs

Check out ICEYE-X59, 66752 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago