INTELSAT 32E (IS-32E) (41945 NORAD) Tracking and Keplerian Element Data
This shows tracking and keplerian element data for the satellite.
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| Element | Value |
| Catalog | 41945 |
| Name | INTELSAT 32E (IS-32E) |
| Epoch Orbit | 3242 |
| Epoch Day | 353.25876513 |
| Epoch Year | 2025 |
| RAAN | 74.0804 |
| Inclination | 0.0325 |
| Eccentricity | 7.1E-05 |
| Argument of Perigee | 315.5885 |
| Mean Anonmoly | 108.4146 |
| Mean Motion | 1.00269829 |
| Decay Rate | -2.44E-06 |
| L1 | 1 41945U 17007B 25353.25876513 -.00000244 00000+0 00000+0 0 9992 |
| L2 | 2 41945 0.0325 74.0804 0000710 315.5885 108.4146 1.00269829 32423 |
Live tracking and technical data element details for INTELSAT 32E (IS-32E) (NORAD 41945). INTELSAT 32E (IS-32E) can be tracked NOW for your location showing map with azimuth and elevation plus other details from your city location.
IsCatalogInMostPopularTable: catalog: 41945, numindb: 1129
Update: records affected: 1
GetName: 41945 INTELSAT 32E (IS-32E)
Hit Count: updated at: Sat, 18 Apr 2026 16:56:21 GMT