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). Payloads include a variety of satellites, spacecraft, and rockets 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.
Focus sentinelFocus sentinel
60508 intel report
Loading greatness...
EAGLEEYE details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 22 hours ago |
| Origin | |
| Manufacturer | CREO |
| Mission | Operational spacecraft |
| Bus & Motor | HYPERSAT, Unknown motor |
| Mass | 55 kg wet, 55 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 22 hours ago
0 EAGLEEYE
1 60508U 24149AS 24287.72207869 .00018546 00000-0 83815-3 0 9995
2 60508 97.4351 2.4295 0004225 298.5594 61.5216 15.20989543 8798Epoch: 2024-10-13T17:19Z
Definitive object data (Epoch: 2024-10-13T17:19:47.598Z)
| Latitude | -0.00005° |
| Longitude | 79.72169° |
| Altitude | 504.56 km |
| Speed | 7.613 km/s |
| True Right ascension | 00h 09m 43s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Predictive object data (real-time)
| Latitude | -47.28315° |
| Longitude | -107.47352° |
| Altitude | 520.016 km |
| Speed | 7.603 km/s |
| Apparent Right ascension | 16h 49m 40s |
| Apparent Declination | -72° 54' 42" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 09:25:18 |
| Azimuth | 157.603° S |
| Elevation | -43.982° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 502.726 km |
| Perigee | 496.914 km |
| Semi-major axis | 6,877.957 km |
| Eccentricity | 0.0004225 |
| Inclination | 97.4351° |
| RAAN | 2.4295° |
| Arg. of periapsis | 298.5594° |
| True anomaly | 61.56417° |
| Mean anomaly | 61.5216° |
| Eccentric anomaly | 61.54288° |
| Mean motion | 3.80499 °/min |
| BSTAR | 0.00083815 |
| Period | 94.61 mins |
No data available
No data available
Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
EAGLEEYE Visibility forecast
Observer location: 39.9160978°, -105.1181434
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 | 2024-10-14 17:35:12.790Z | 34.657° NE | 2024-10-14 17:38:12.790Z | 116.149° SE | 31.077° | 2024-10-14 17:41:12.790Z | 168.224° S |
| 4 mins | 2024-10-15 05:47:12.790Z | 217.429° SW | 2024-10-15 05:49:12.790Z | 271.545° WNW | 26.326° | 2024-10-15 05:51:12.790Z | 316.056° NNW |