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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60508 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PL / POLRelated business
Manufacturer
CREO
Mission
Operational Commercial Imaging
Bus & Motor
HYPERSAT, Unknown motor
Mass
55 kg wet, 55 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
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 & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 EAGLEEYE
1 60508U 24149AS 25261.79251548 .00024097 00000-0 62588-3 0 9990
2 60508 97.4019 342.1784 0004823 158.3602 201.7849 15.38946835 60810Epoch: 2025-09-18T19:01Z
TLE epoch observation values (Epoch: 2025-09-18T19:01:13.337Z)
Latitude
0.00007°
Longitude
58.92379°
Altitude
455.397 km
Speed
7.638 km/s
True Right ascension
22h 48m 42s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
02:44:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
449.454 km
Perigee altitude
442.871 km
Semi-major axis
6,824.3 km
Eccentricity
0.00048
Inclination
97.4019°
RAAN
342.1784°
Arg. of periapsis
158.3602°
True anomaly
201.7644°
Mean anomaly
201.7849°
Eccentric anomaly
201.77465°
Mean motion
3.84996 °/min
Orbital period
93.51 mins
BSTAR
0.00062588
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
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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.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 | 2025-09-20 05:29:34.595Z | 165.525° S | 2025-09-20 05:31:34.595Z | 41.72° NE | 44.935° | 2025-09-20 05:34:34.595Z | 348.888° N |
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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