INTELSAT 17 (IS-17) is a payload in GEO orbit, operated by Intelsat S.A., US headquarters, launched 2010.
| Orbit class | GEO |
| Inclination | 0.0081° |
| Eccentricity | 0.0002595 |
| Period | 1436.1 min |
| Apogee | 35,797 km |
| Perigee | 35,775 km |
| Mean motion | 1.00272512 rev/day |
| RAAN | 71.7599° |
| Arg of perigee | 39.3646° |
| Mean anomaly | 296.9251° |
| B* | 0.0000e+0 |
| Rev at epoch | 5,344 |
1 37238U 10065B 26188.15814794 .00000013 00000-0 00000-0 0 99932 37238 0.0081 71.7599 0002595 39.3646 296.9251 1.00272512 53444{
"OBJECT_NAME": "INTELSAT 17 (IS-17)",
"OBJECT_ID": "2010-065B",
"EPOCH": "2026-07-07T03:47:43.982+00:00",
"MEAN_MOTION": 1.00272512,
"ECCENTRICITY": 0.0002595,
"INCLINATION": 0.0081,
"RA_OF_ASC_NODE": 71.7599,
"ARG_OF_PERICENTER": 39.3646,
"MEAN_ANOMALY": 296.9251,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 37238,
"REV_AT_EPOCH": 5344,
"BSTAR": 0,
"MEAN_MOTION_DOT": 1.3e-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 | INTELSAT 17 (IS-17) |
| 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 |