INTELSAT 32E (IS-32E) is a payload in GEO orbit, operated by DirecTV Latin America / Intelsat S.A., US headquarters, launched 2017.
| Orbit class | GEO |
| Inclination | 0.0160° |
| Eccentricity | 0.0000740 |
| Period | 1436.1 min |
| Apogee | 35,790 km |
| Perigee | 35,784 km |
| Mean motion | 1.00269679 rev/day |
| RAAN | 332.9685° |
| Arg of perigee | 11.3752° |
| Mean anomaly | 327.3135° |
| B* | 0.0000e+0 |
| Rev at epoch | 3,442 |
1 41945U 17007B 26188.19350479 -.00000254 00000-0 00000-0 0 99932 41945 0.0160 332.9685 0000740 11.3752 327.3135 1.00269679 34425{
"OBJECT_NAME": "INTELSAT 32E (IS-32E)",
"OBJECT_ID": "2017-007B",
"EPOCH": "2026-07-07T04:38:38.814+00:00",
"MEAN_MOTION": 1.00269679,
"ECCENTRICITY": 0.000074,
"INCLINATION": 0.016,
"RA_OF_ASC_NODE": 332.9685,
"ARG_OF_PERICENTER": 11.3752,
"MEAN_ANOMALY": 327.3135,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 41945,
"REV_AT_EPOCH": 3442,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.00000254,
"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 32E (IS-32E) |
| Operator | DirecTV Latin America / Intelsat S.A., US headquartersHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree |
| Country | |
| Launch date | |
| Launch mass (kg) | 6300HIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Mission purpose | — |
| Object class |
| Orbital regime |
| Status |