FOSSASAT-2E25 is a payload in SSO orbit, operated by Fossa Systems, launched 2026.
| Orbit class | SSO |
| Inclination | 97.7608° |
| Eccentricity | 0.0001431 |
| Period | 96.5 min |
| Apogee | 592 km |
| Perigee | 590 km |
| Mean motion | 14.92165882 rev/day |
| RAAN | 145.6826° |
| Arg of perigee | 162.7067° |
| Mean anomaly | 197.4201° |
| B* | 7.6810e-5 |
| Rev at epoch | 1,463 |
1 68478U 26067BQ 26187.67884977 .00000726 00000-0 76810-4 0 99952 68478 97.7608 145.6826 0001431 162.7067 197.4201 14.92165882 14636{
"OBJECT_NAME": "FOSSASAT-2E25",
"OBJECT_ID": "2026-067BQ",
"EPOCH": "2026-07-06T16:17:32.62+00:00",
"MEAN_MOTION": 14.92165882,
"ECCENTRICITY": 0.0001431,
"INCLINATION": 97.7608,
"RA_OF_ASC_NODE": 145.6826,
"ARG_OF_PERICENTER": 162.7067,
"MEAN_ANOMALY": 197.4201,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 68478,
"REV_AT_EPOCH": 1463,
"BSTAR": 0.00007681,
"MEAN_MOTION_DOT": 0.00000726,
"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 | FOSSASAT-2E25 |
| Operator | |
| Country | Spain |
| 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 |