GSAT0102 (GALILEO-FM2) is a payload in MEO orbit, operated by European Space Agency / European Global Navigation Satellite Systems Agency, launched 2011.
Orbital data last updated 3 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | MEO |
| Inclination | 56.9894° |
| Eccentricity | 0.0002522 |
| Period | 844.7 min |
| Apogee | 23,229 km |
| Perigee | 23,215 km |
| Mean motion | 1.70476028 rev/day |
| RAAN | 341.3121° |
| Arg of perigee | 12.9231° |
| Mean anomaly | 348.3249° |
| B* | 0.0000e+0 |
| Rev at epoch | 9,141 |
1 37847U 11060B 26184.78699916 -.00000075 00000-0 00000-0 0 99962 37847 56.9894 341.3121 0002522 12.9231 348.3249 1.70476028 91419{
"OBJECT_NAME": "GSAT0102 (GALILEO-FM2)",
"OBJECT_ID": "2011-060B",
"EPOCH": "2026-07-03T18:53:16.727+00:00",
"MEAN_MOTION": 1.70476028,
"ECCENTRICITY": 0.0002522,
"INCLINATION": 56.9894,
"RA_OF_ASC_NODE": 341.3121,
"ARG_OF_PERICENTER": 12.9231,
"MEAN_ANOMALY": 348.3249,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 37847,
"REV_AT_EPOCH": 9141,
"BSTAR": 0,
"MEAN_MOTION_DOT": -7.5e-7,
"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 | GSAT0102 (GALILEO-FM2) |
| Operator | European Space Agency / European Global Navigation Satellite Systems AgencyHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | ESA |
| Launch date | |
| Launch mass (kg) |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |