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EAGLEEYE, 60508

Orbit data source: Space-Track

EAGLEEYE, 60508 is a Polish payload satellite in SSO that was launched on Fri, 16 Aug 2024 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

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Iframe URL

https://www.satcat.com/sats-embedded/60508?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

60508, 2024-149AS

Orbit

SSO

Country

PL / POL

Related business

Creotech Instruments S.A. (PL)

Manufacturer

CREO

Mission

Operational Commercial Imaging

Bus & Motor

HYPERSAT, Unknown motor

Mass

55 kg wet, 55 kg dry

Launch date (UTC)

2024-08-16 (2 years ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 0.8 m

Radar Cross Section

0.714 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago

0 EAGLEEYE
1 60508U 24149AS  26256.79289852  .00688647  24003-3  94974-3 0  9997
2 60508  97.3534 356.6479 0007313 262.1295  97.9157 16.06095714116952

Epoch: 2026-09-13T19:01Z

TLE epoch observation values (Epoch: 2026-09-13T19:01:46.432Z)

Latitude

0.00005°

Longitude

78.42197°

Altitude

261.455 km

Speed

7.75 km/s

True Right ascension

23h 46m 35s

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

15:25:22

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

259.276 km

Perigee altitude

249.575 km

Semi-major axis

6,632.562 km

Eccentricity

0.00073

Inclination

97.3534°

RAAN

356.6479°

Arg. of periapsis

262.1295°

True anomaly

97.99869°

Mean anomaly

97.9157°

Eccentric anomaly

97.9572°

Mean motion

4.0181 °/min

Orbital period

89.59 mins

BSTAR

0.00094974

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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)

TROOP-F2, 60557 (Decayed)

FLOCK 4BE 28, 60519

CONNECTA IOT-4, 60524

FLOCK 4BE 7, 60481

LEMUR 2 SQUIRRELCOMM, 60578

OBJECT BQ, 60530

PICO-02D024, 60569 (Decayed)

TOMORROW-S1, 60479

ICEYE-X39, 60546

SATELIOT_1, 60550

PHISAT 2, 60470

FLOCK 4BE 17, 60492

PTD-R (TYVAK-0127), 60523 (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

EAGLEEYE 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.
EAGLEEYE 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 EAGLEEYE, 60508 on other resources

View EAGLEEYE, 60508 on NASA - NSSDCA Website

View EAGLEEYE, 60508 on Heavens-Above

View EAGLEEYE, 60508 on Keep Track

View EAGLEEYE, 60508 on Celestrak

View EAGLEEYE, 60508 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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