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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

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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 (2 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  25299.65582557  .00037037  00000-0  47466-3 0  9994
2 56961  97.5732  80.1519 0000776  79.6016 280.5327 15.59088973132531

Epoch: 2025-10-26T15:44Z

TLE epoch observation values (Epoch: 2025-10-26T15:44:23.329Z)

Latitude

-0.00003°

Longitude

168.7858°

Altitude

393.335 km

Speed

7.674 km/s

True Right ascension

05h 20m 36s

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

20:24:53

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

387.739 km

Perigee altitude

386.689 km

Semi-major axis

6,765.351 km

Eccentricity

0.00008

Inclination

97.5732°

RAAN

80.1519°

Arg. of periapsis

79.6016°

True anomaly

280.52396°

Mean anomaly

280.5327°

Eccentric anomaly

280.52833°

Mean motion

3.90039 °/min

Orbital period

92.3 mins

BSTAR

0.00047466

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

OBJECT CA, 60449

FOSSASAT2E16 (FEROX), 56932 (Decayed)

LEMUR 2 AADAM-ALIYAH, 56977 (Decayed)

NUSAT-43 (R DIENG-KUNTZ), 56968

DROID-001, 56965

ICEYE-X23, 56949

BLACKJACK ACES-2, 56955

SPACEBEE-178, 56973 (Decayed)

OBJECT P, 56945 (Decayed)

NUSAT-40 (C SHOEMAKER), 56943

NUSAT-42 (M WONENBURGER), 56966

BLACKJACK ACES-4, 56952

ICEYE-X25, 56963

FOSSASAT2E17 (FEROX), 56935 (Decayed)

EIVE, 56937 (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.

Click here to try in Sandbox

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.
4 mins	2025-10-27 08:49:45.870Z	117.31° SE	2025-10-27 08:51:45.870Z	74.971° E	18.016°	2025-10-27 08:53:45.870Z	28.177° NE

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Please sign-in to view Co-orbital & Co-planar RSOs.

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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

Go to standalone docs website

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