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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.

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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

Last TLE update

5 hours ago

Origin

Creotech Instruments S.A. (PL / POL)

Manufacturer

CREO

Mission

Operational Commercial Imaging

Bus & Motor

HYPERSAT, Unknown motor

Mass

55 kg wet, 55 kg dry

Launch date (UTC)

2024-08-16 (11 months ago)

Launch vehicle

FALCON 9

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Box + 2 Pan, 1.5 m

Radar Cross Section

0.714 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 5 hours ago

0 EAGLEEYE
1 60508U 24149AS  25194.16066281  .00016892  00000-0  48537-3 0  9996
2 60508  97.4070 274.0345 0005034  64.4935 295.6829 15.35881572 50423

Epoch: 2025-07-13T03:51Z

TLE epoch observation values (Epoch: 2025-07-13T03:51:21.266Z)

Latitude

-0.00003°

Longitude

-75.09197°

Altitude

459.925 km

Speed

7.638 km/s

True Right ascension

18h 16m 08s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

79.96602°

Longitude

-121.82209°

Altitude

468.395 km

Speed

7.641 km/s

Apparent Right ascension

10h 14m 10s

Apparent Declination

27° 27' 55"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

21:19:55

Azimuth

347.082° N

Elevation

-21.446°

Doppler factor

Orbital elements

Apogee altitude

458.688 km

Perigee altitude

451.808 km

Semi-major axis

6,833.385 km

Eccentricity

0.0005

Inclination

97.407°

RAAN

274.0345°

Arg. of periapsis

64.4935°

True anomaly

Unknown

Mean anomaly

295.6829°

Eccentric anomaly

Unknown

Mean motion

3.84228 °/min

Orbital period

93.69 mins

BSTAR

0.00048537

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

OBJECT A, 60468

FLOCK 4BE 17, 60492

NUSAT-50 (NANCY ROMAN), 60493

NUSAT-48 (H. LEAVITT), 60498

FLOCK 4BE 30, 60499

NUSAT-49(K.VON NEUMANN), 60500

EAGLEEYE Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-13 18:29:25.408Z	357.621° N	2025-07-13 18:31:25.408Z	315.578° NNW	36.568°	2025-07-13 18:34:25.408Z	211.51° SW
4 mins	2025-07-14 05:01:25.408Z	130.85° SE	2025-07-14 05:03:25.408Z	61.765° ENE	32.181°	2025-07-14 05:05:25.408Z	10.78° NNE

Authenticating...

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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.