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

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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 (1 year 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: 19 hours ago

TLE from 19 hours ago

0 EAGLEEYE
1 60508U 24149AS  25339.19159867  .00061052  00000-0  12443-2 0  9997
2 60508  97.3943  60.6907 0003007 237.7090 122.3868 15.46021303 72747

Epoch: 2025-12-05T04:35Z

TLE epoch observation values (Epoch: 2025-12-05T04:35:54.125Z)

Latitude

-0.00002°

Longitude

-82.52205°

Altitude

432.602 km

Speed

7.651 km/s

True Right ascension

04h 02m 45s

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

22:03:24

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

427.355 km

Perigee altitude

423.264 km

Semi-major axis

6,803.447 km

Eccentricity

0.0003

Inclination

97.3943°

RAAN

60.6907°

Arg. of periapsis

237.709°

True anomaly

122.41589°

Mean anomaly

122.3868°

Eccentric anomaly

122.40135°

Mean motion

3.86767 °/min

Orbital period

93.08 mins

BSTAR

0.0012443

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

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EAGLEEYE 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.
6 mins	2025-12-06 05:34:43.789Z	162.614° S	2025-12-06 05:37:43.789Z	33.844° NE	43.867°	2025-12-06 05:40:43.789Z	350.925° N
5 mins	2025-12-06 18:26:43.789Z	15.068° NNE	2025-12-06 18:28:43.789Z	68.173° E	44.63°	2025-12-06 18:31:43.789Z	190.047° SSW

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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 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.

EAGLEEYE, 60508

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2025-12-05T04:35:54.125Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

EAGLEEYE Visibility forecast

Co-orbital & Co-planar RSOs

Check out EAGLEEYE, 60508 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 19 hours ago