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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

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: 20 hours ago

TLE from 20 hours ago

0 EAGLEEYE
1 60508U 24149AS  25257.50076848  .00022083  00000-0  57823-3 0  9991
2 60508  97.4011 337.8460 0004643 171.4161 188.7164 15.38716724 60153

Epoch: 2025-09-14T12:01Z

TLE epoch observation values (Epoch: 2025-09-14T12:01:06.396Z)

Latitude

-0.00009°

Longitude

163.85048°

Altitude

456.153 km

Speed

7.637 km/s

True Right ascension

22h 31m 23s

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

00:50:52

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

450.013 km

Perigee altitude

443.675 km

Semi-major axis

6,824.981 km

Eccentricity

0.00046

Inclination

97.4011°

RAAN

337.846°

Arg. of periapsis

171.4161°

True anomaly

188.70834°

Mean anomaly

188.7164°

Eccentric anomaly

188.71237°

Mean motion

3.84938 °/min

Orbital period

93.52 mins

BSTAR

0.00057823

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Computing Atmospheric mass density...

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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

FLOCK 4BE 22, 60494

FLOCK 4BE 34, 60495

FLOCK 4BE 32, 60497

NUSAT-48 (H. LEAVITT), 60498

FLOCK 4BE 30, 60499

NUSAT-49(K.VON NEUMANN), 60500

FLOCK 4BE 11, 60501

FLOCK 4BE 33, 60502

FLOCK 4BE 10, 60503

FLOCK 4BE 24, 60505

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 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	2025-09-15 18:14:09.445Z	16.942° NNE	2025-09-15 18:17:09.445Z	162.424° S	41.207°	2025-09-15 18:19:09.445Z	186.037° SSW

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Please sign-in to view Co-orbital & Co-planar RSOs.

Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in ascending order

CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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.

Documentation

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