EAGLEEYE is a payload in SSO orbit, operated by Creotech Instruments S.A., launched 2024.
| Orbit class | SSO |
| Inclination | 97.3713° |
| Eccentricity | 0.0004999 |
| Period | 91.4 min |
| Apogee | 348 km |
| Perigee | 341 km |
| Mean motion | 15.75020003 rev/day |
| RAAN | 281.7014° |
| Arg of perigee | 202.6773° |
| Mean anomaly | 157.4271° |
| B* | 8.4974e-4 |
| Rev at epoch | 10,593 |
1 60508U 24149AS 26187.25783419 .00127660 00000-0 84974-3 0 99992 60508 97.3713 281.7014 0004999 202.6773 157.4271 15.75020003105930{
"OBJECT_NAME": "EAGLEEYE",
"OBJECT_ID": "2024-149AS",
"EPOCH": "2026-07-06T06:11:16.874+00:00",
"MEAN_MOTION": 15.75020003,
"ECCENTRICITY": 0.00049986,
"INCLINATION": 97.3713,
"RA_OF_ASC_NODE": 281.7014,
"ARG_OF_PERICENTER": 202.6773,
"MEAN_ANOMALY": 157.4271,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 60508,
"REV_AT_EPOCH": 10593,
"BSTAR": 0.00084974082,
"MEAN_MOTION_DOT": 0.0012766,
"MEAN_MOTION_DDOT": 0
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | EAGLEEYE |
| Operator | |
| Country | Poland |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |