INTELSAT 902 (IS-902) is a payload in GEO orbit, operated by Intelsat Ltd, US headquarters, launched 2001.
| Orbit class | GEO |
| Inclination | 6.1655° |
| Eccentricity | 0.0004302 |
| Period | 1436.1 min |
| Apogee | 35,805 km |
| Perigee | 35,769 km |
| Mean motion | 1.00270287 rev/day |
| RAAN | 71.5417° |
| Arg of perigee | 32.4645° |
| Mean anomaly | 97.8422° |
| B* | 0.0000e+0 |
| Rev at epoch | 9,089 |
1 26900U 01039A 26187.90857824 -.00000272 00000-0 00000-0 0 99992 26900 6.1655 71.5417 0004302 32.4645 97.8422 1.00270287 90895{
"OBJECT_NAME": "INTELSAT 902 (IS-902)",
"OBJECT_ID": "2001-039A",
"EPOCH": "2026-07-06T21:48:21.16+00:00",
"MEAN_MOTION": 1.00270287,
"ECCENTRICITY": 0.0004302,
"INCLINATION": 6.1655,
"RA_OF_ASC_NODE": 71.5417,
"ARG_OF_PERICENTER": 32.4645,
"MEAN_ANOMALY": 97.8422,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 26900,
"REV_AT_EPOCH": 9089,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000272,
"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 | INTELSAT 902 (IS-902) |
| Operator | |
| Country | United States |
| 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 |