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ICEYE-X26, 56961

Orbit data source: Space-Track

ICEYE-X26, 56961 is a payload satellite owned by ICEYE US (US) in LEO that was launched on Mon, 12 Jun 2023 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/56961?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/56961?theme=dark&initialShowStats=false

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ISO8601 Format

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ISO8601 Format

Identifier

56961, 2023-084AF

Orbit

LEO

Country

US

Related business

Manufacturer

ICEYE

Mission

Decayed Commercial Radar Imaging

Bus & Motor

ICEYE, Unknown motor

Mass

90 kg wet, 89 kg dry

Launch date (UTC)

2023-06-12 (3 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 1 Pan, 1.6 m

Radar Cross Section

0.825 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 days ago

TLE from 6 days ago

0 ICEYE-X26
1 56961U 23084AF  26151.53340426  .07996038  26164-5  98774-3 0  9990
2 56961  97.5464 315.9673 0014332 270.4834  89.4821 16.35905726166626

Epoch: 2026-05-31T12:48Z

TLE epoch observation values (Epoch: 2026-05-31T12:48:06.128Z)

Latitude

0.00005°

Longitude

-125.09195°

Altitude

179.886 km

Speed

7.798 km/s

True Right ascension

21h 03m 52s

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

13:58:13

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

182.926 km

Perigee altitude

164.146 km

Semi-major axis

6,551.673 km

Eccentricity

0.00143

Inclination

97.5464°

RAAN

315.9673°

Arg. of periapsis

270.4834°

True anomaly

89.64633°

Mean anomaly

89.4821°

Eccentric anomaly

89.56421°

Mean motion

4.09275 °/min

Orbital period

87.96 mins

BSTAR

0.00098774

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Other satellites on launch #84 in the year 2023 (2023-06-12 UTC)

NUSAT-43 (R DIENG-KUNTZ), 56968 (Decayed)

AFRL-XVI, 56942 (Decayed)

NUSAT-41 (C PAYNE-G), 56944

GEISAT PRECURSOR, 56934

BLACKJACK ACES-4, 56952 (Decayed)

OBJECT K, 56941 (Decayed)

ICEYE-X25, 56963

AAC-AIS-SAT2, 56996

SKYKRAFT-3, 56229 (Decayed)

OBJECT BQ, 56231 (Decayed)

SPEI SATELLES, 56991 (Decayed)

TOMORROW-R2, 56962

SPACEBEE-177, 56972 (Decayed)

ION SCV-011, 56957

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

ICEYE-X26 Visibility

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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.
ICEYE-X26 is likely not visible in the next few days.

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-X26, 56961 on other resources

View ICEYE-X26, 56961 on NASA - NSSDCA Website

View ICEYE-X26, 56961 on Heavens-Above

View ICEYE-X26, 56961 on Keep Track

View ICEYE-X26, 56961 on Celestrak

View ICEYE-X26, 56961 on Gunter's Space Page

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

Documentation

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