[−][src]Struct sgp4::Prediction
Predicted satellite position and velocity after SGP4 propagation
The position and velocity are given in the True Equator, Mean Equinox (TEME) of epoch reference frame.
Fields
position: [f64; 3]
The three position components (x, y, z) in km
velocity: [f64; 3]
The three velocity components (x, y, z) in km.s⁻¹
Auto Trait Implementations
impl RefUnwindSafe for Prediction
impl Send for Prediction
impl Sync for Prediction
impl Unpin for Prediction
impl UnwindSafe for Prediction
Blanket Implementations
impl<T> Any for T where
T: 'static + ?Sized,
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T: 'static + ?Sized,
impl<T> Borrow<T> for T where
T: ?Sized,
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T: ?Sized,
impl<T> BorrowMut<T> for T where
T: ?Sized,
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T: ?Sized,
fn borrow_mut(&mut self) -> &mut T
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impl<T> From<T> for T
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impl<T, U> Into<U> for T where
U: From<T>,
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U: From<T>,
impl<T, U> TryFrom<U> for T where
U: Into<T>,
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U: Into<T>,
type Error = Infallible
The type returned in the event of a conversion error.
fn try_from(value: U) -> Result<T, <T as TryFrom<U>>::Error>
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impl<T, U> TryInto<U> for T where
U: TryFrom<T>,
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U: TryFrom<T>,