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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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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: 11 hours ago

TLE from 11 hours ago

0 EAGLEEYE
1 60508U 24149AS  26097.72556617  .00065593  00000-0  77879-3 0  9991
2 60508  97.3731 187.7724 0003743 161.5612 198.5782 15.60969251 91910

Epoch: 2026-04-07T17:24Z

TLE epoch observation values (Epoch: 2026-04-07T17:24:48.917Z)

Latitude

0.00003°

Longitude

90.57042°

Altitude

390.403 km

Speed

7.675 km/s

True Right ascension

12h 31m 05s

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

10:59:50

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

384.296 km

Perigee altitude

379.236 km

Semi-major axis

6,759.903 km

Eccentricity

0.00037

Inclination

97.3731°

RAAN

187.7724°

Arg. of periapsis

161.5612°

True anomaly

198.56454°

Mean anomaly

198.5782°

Eccentric anomaly

198.57137°

Mean motion

3.9051 °/min

Orbital period

92.19 mins

BSTAR

0.00077879

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

LEMUR 2 TOMATOKECHUP, 60471

PICO-02G027, 60566 (Decayed)

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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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.
5 mins	2026-04-08 05:51:25.745Z	154.968° SSE	2026-04-08 05:53:25.745Z	108.269° ESE	40.218°	2026-04-08 05:56:25.745Z	355.697° N
4 mins	2026-04-08 18:36:25.745Z	40.078° NE	2026-04-08 18:37:25.745Z	82.094° E	36.085°	2026-04-08 18:40:25.745Z	175.996° S

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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: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-04-07T17:24:48.917Z)

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: 11 hours ago