| Display title | Astronomy:Simplified perturbations models |
| Default sort key | Simplified perturbations models |
| Page length (in bytes) | 6,019 |
| Namespace ID | 3024 |
| Namespace | Astronomy |
| Page ID | 260279 |
| Page content language | en - English |
| Page content model | wikitext |
| Indexing by robots | Allowed |
| Number of redirects to this page | 0 |
| Counted as a content page | Yes |
| HandWiki item ID | None |
| Edit | Allow all users (infinite) |
| Move | Allow all users (infinite) |
| Page creator | imported>WikiGary |
| Date of page creation | 08:28, 6 February 2024 |
| Latest editor | imported>WikiGary |
| Date of latest edit | 08:28, 6 February 2024 |
| Total number of edits | 1 |
| Recent number of edits (within past 90 days) | 0 |
| Recent number of distinct authors | 0 |
Description | Content |
Article description: (description)
This attribute controls the content of the description and og:description elements. | Simplified perturbations models are a set of five mathematical models (SGP, SGP4, SDP4, SGP8 and SDP8) used to calculate orbital state vectors of satellites and space debris relative to the Earth-centered inertial coordinate system. This set of models is often referred to collectively as SGP4 due to... |
