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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 SSO 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.

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Iframe URL

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

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ISO8601 Format

Identifier

56961, 2023-084AF

Orbit

SSO

Country

US

Related business

Manufacturer

ICEYE

Mission

Operational 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: 9 hours ago

TLE from 9 hours ago

0 ICEYE-X26
1 56961U 23084AF  25354.89116992  .00031838  00000-0  33663-3 0  9995
2 56961  97.5731 139.1973 0000483 144.8032 215.3258 15.64126424141154

Epoch: 2025-12-20T21:23Z

TLE epoch observation values (Epoch: 2025-12-20T21:23:17.081Z)

Latitude

-0.00004°

Longitude

88.66467°

Altitude

379.164 km

Speed

7.682 km/s

True Right ascension

09h 16m 47s

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

05:03:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

372.993 km

Perigee altitude

372.341 km

Semi-major axis

6,750.804 km

Eccentricity

0.00005

Inclination

97.5731°

RAAN

139.1973°

Arg. of periapsis

144.8032°

True anomaly

215.3226°

Mean anomaly

215.3258°

Eccentric anomaly

215.3242°

Mean motion

3.913 °/min

Orbital period

92 mins

BSTAR

0.00033663

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

MUSAT1, 56967 (Decayed)

AYRIS-2, 56986 (Decayed)

ELO-4, 56990 (Decayed)

SPACEBEE-177, 56972 (Decayed)

SPACEBEE-169, 56982 (Decayed)

SPACEBEE-178, 56973 (Decayed)

SPEI SATELLES, 56991 (Decayed)

AYRIS-1, 56988 (Decayed)

MRC-100, 56993 (Decayed)

OBJECT BW, 56994 (Decayed)

AII-DELTA, 56987 (Decayed)

SPACEBEE-168, 56984 (Decayed)

SPACEBEE-171, 56980 (Decayed)

EIVE, 56937 (Decayed)

OBJECT BR, 56989 (Decayed)

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.

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ICEYE-X26 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.
5 mins	2025-12-21 09:48:04.878Z	163.873° S	2025-12-21 09:51:04.878Z	0.999° NNE	40.311°	2025-12-21 09:53:04.878Z	350.145° 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-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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