INTELSAT 25 (IS-25) is a payload in GEO orbit, operated by Protostar Ltd, launched 2008.
Orbital data last updated 25 days ago. This may not reflect the current orbital state — not for operational use or collision avoidance.
| Orbit class | GEO |
| Inclination | 2.6965° |
| Eccentricity | 0.0003046 |
| Period | 1454.0 min |
| Apogee | 36,149 km |
| Perigee | 36,123 km |
| Mean motion | 0.99037089 rev/day |
| RAAN | 80.4270° |
| Arg of perigee | 56.5758° |
| Mean anomaly | 12.5794° |
| B* | 0.0000e+0 |
| Rev at epoch | 6,564 |
1 33153U 08034A 26163.20981263 -.00000270 00000-0 00000-0 0 99992 33153 2.6965 80.4270 0003046 56.5758 12.5794 0.99037089 65649{
"OBJECT_NAME": "INTELSAT 25 (IS-25)",
"OBJECT_ID": "2008-034A",
"EPOCH": "2026-06-12T05:02:07.811+00:00",
"MEAN_MOTION": 0.99037089,
"ECCENTRICITY": 0.00030455,
"INCLINATION": 2.6965,
"RA_OF_ASC_NODE": 80.427,
"ARG_OF_PERICENTER": 56.5758,
"MEAN_ANOMALY": 12.5794,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 33153,
"REV_AT_EPOCH": 6564,
"BSTAR": 0,
"MEAN_MOTION_DOT": -0.0000027,
"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 25 (IS-25) |
| Operator | |
| Country | BM |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |