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 | 2679 |
| Epoch Day | 158.41192519 |
| Epoch Year | 2024 |
| RAAN | 40.1989 |
| Inclination | 0.0149 |
| Eccentricity | 4.41E-05 |
| Argument of Perigee | 264.2736 |
| Mean Anonmoly | 55.9373 |
| Mean Motion | 1.00269348 |
| Decay Rate | -2.67E-06 |
| L1 | 1 41945U 17007B 24158.41192519 -.00000267 00000+0 00000+0 0 9994 |
| L2 | 2 41945 0.0149 40.1989 0000441 264.2736 55.9373 1.00269348 26798 |
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: 850
Update: records affected: 1
GetName: 41945 INTELSAT 32E (IS-32E)
Hit Count: updated at: Tue, 17 Sep 2024 12:31:59 GMT