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 | 2925 |
| Epoch Day | 35.04650625 |
| Epoch Year | 2025 |
| RAAN | 88.9222 |
| Inclination | 0.0161 |
| Eccentricity | 3E-06 |
| Argument of Perigee | 42.0078 |
| Mean Anonmoly | 337.0682 |
| Mean Motion | 1.00269064 |
| Decay Rate | -2.65E-06 |
| L1 | 1 41945U 17007B 25035.04650625 -.00000265 00000+0 00000+0 0 9993 |
| L2 | 2 41945 0.0161 88.9222 0000030 42.0078 337.0682 1.00269064 29253 |
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: 949
Update: records affected: 1
GetName: 41945 INTELSAT 32E (IS-32E)
Hit Count: updated at: Thu, 19 Jun 2025 09:52:21 GMT