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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

11 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 11 hours ago

0 EAGLEEYE
1 60508U 24149AS  25182.75792859  .00015565  00000-0  45239-3 0  9997
2 60508  97.4066 262.5672 0005645  96.0631 264.1256 15.35538197 48676

Epoch: 2025-07-01T18:11Z

TLE epoch observation values (Epoch: 2025-07-01T18:11:25.03Z)

Latitude

0°

Longitude

69.66412°

Altitude

462.831 km

Speed

7.635 km/s

True Right ascension

17h 30m 16s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-75.59941°

Longitude

-140.12662°

Altitude

490.37 km

Speed

7.616 km/s

Apparent Right ascension

04h 09m 33s

Apparent Declination

-58° 24' 58"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

16:22:57

Azimuth

174.503° S

Elevation

-71.376°

Doppler factor

Orbital elements

Apogee altitude

460.126 km

Perigee altitude

452.41 km

Semi-major axis

6,834.405 km

Eccentricity

0.00056

Inclination

97.4066°

RAAN

262.5672°

Arg. of periapsis

96.0631°

True anomaly

Unknown

Mean anomaly

264.1256°

Eccentric anomaly

Unknown

Mean motion

3.84142 °/min

Orbital period

93.72 mins

BSTAR

0.00045239

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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.
6 mins	2025-07-02 05:15:30.710Z	160.345° S	2025-07-02 05:18:30.710Z	120.846° SE	42.099°	2025-07-02 05:21:30.710Z	353.923° N
5 mins	2025-07-02 18:13:30.710Z	12.433° NNE	2025-07-02 18:15:30.710Z	189.245° SSW	44.558°	2025-07-02 18:18:30.710Z	192.724° SSW

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.