INMARSAT 3-F2 is a payload in GEO orbit, operated by International Maritime Satellite Organization, launched 1996.
| Orbit class | GEO |
| Inclination | 9.9005° |
| Eccentricity | 0.0006439 |
| Period | 1440.1 min |
| Apogee | 35,891 km |
| Perigee | 35,837 km |
| Mean motion | 0.99995844 rev/day |
| RAAN | 53.7335° |
| Arg of perigee | 46.9335° |
| Mean anomaly | 298.7784° |
| B* | 0.0000e+0 |
| Rev at epoch | 10,911 |
1 24307U 96053A 26187.95698301 -.00000345 00000-0 00000-0 0 99972 24307 9.9005 53.7335 0006439 46.9335 298.7784 0.99995844109113{
"OBJECT_NAME": "INMARSAT 3-F2",
"OBJECT_ID": "1996-053A",
"EPOCH": "2026-07-06T22:58:03.332+00:00",
"MEAN_MOTION": 0.99995844,
"ECCENTRICITY": 0.0006439,
"INCLINATION": 9.9005,
"RA_OF_ASC_NODE": 53.7335,
"ARG_OF_PERICENTER": 46.9335,
"MEAN_ANOMALY": 298.7784,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 24307,
"REV_AT_EPOCH": 10911,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000345,
"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 | INMARSAT 3-F2 |
| Operator | |
| Country | Inmarsat |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |