FOSSASAT-2E19 (TAT-E) is a payload in SSO orbit, operated by Fossa Systems, launched 2025.
| Orbit class | SSO |
| Inclination | 97.3953° |
| Eccentricity | 0.0003483 |
| Period | 94.7 min |
| Apogee | 505 km |
| Perigee | 500 km |
| Mean motion | 15.21250076 rev/day |
| RAAN | 265.6411° |
| Arg of perigee | 267.8420° |
| Mean anomaly | 92.2417° |
| B* | 1.1157e-4 |
| Rev at epoch | 8,166 |
1 62676U 25009BV 26187.71134528 .00002423 00000-0 11157-3 0 99972 62676 97.3953 265.6411 0003483 267.8420 92.2417 15.21250076 81662{
"OBJECT_NAME": "FOSSASAT-2E19 (TAT-E)",
"OBJECT_ID": "2025-009BV",
"EPOCH": "2026-07-06T17:04:20.232+00:00",
"MEAN_MOTION": 15.21250076,
"ECCENTRICITY": 0.0003483,
"INCLINATION": 97.3953,
"RA_OF_ASC_NODE": 265.6411,
"ARG_OF_PERICENTER": 267.842,
"MEAN_ANOMALY": 92.2417,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 62676,
"REV_AT_EPOCH": 8166,
"BSTAR": 0.00011157,
"MEAN_MOTION_DOT": 0.00002423,
"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-2E19 (TAT-E) |
| 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 |