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: 19 hours ago
TLE from 19 hours ago
0 EAGLEEYE
1 60508U 24149AS 25324.49205176 .00038552 00000-0 82689-3 0 9998
2 60508 97.3957 45.7199 0002859 302.3802 57.7170 15.44630226 70476Epoch: 2025-11-20T11:48Z
TLE epoch observation values (Epoch: 2025-11-20T11:48:33.272Z)
Latitude
0.00005°
Longitude
168.8326°
Altitude
434.549 km
Speed
7.652 km/s
True Right ascension
03h 02m 52s
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
03:51:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
431.344 km
Perigee altitude
427.451 km
Semi-major axis
6,807.534 km
Eccentricity
0.00029
Inclination
97.3957°
RAAN
45.7199°
Arg. of periapsis
302.3802°
True anomaly
57.7447°
Mean anomaly
57.717°
Eccentric anomaly
57.73085°
Mean motion
3.86419 °/min
Orbital period
93.16 mins
BSTAR
0.00082689
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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 | 2025-11-21 17:54:32.012Z | 35.29° NE | 2025-11-21 17:57:32.012Z | 102.229° ESE | 25.607° | 2025-11-21 17:59:32.012Z | 151.582° SSE |
| 5 mins | 2025-11-22 05:55:32.012Z | 194.376° SSW | 2025-11-22 05:57:32.012Z | 266.487° W | 35.88° | 2025-11-22 06:00:32.012Z | 335.458° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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 |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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