Enum OrbitClass 

pub enum OrbitClass {
    MeoGnss,
    Geosynchronous,
    Leo,
}

Orbit class supplying a physical earth-fixed displacement bound.

Each bound is sqrt(mu / a_min) + omega_earth * r_max, the inertial speed at the class’s tightest published semi-major axis plus the largest possible earth-rotation transport term at its widest radius. That sum is a true upper bound on earth-fixed speed for any geometry in the class, so the gate cannot false-positive on physically real data. It is correspondingly loose - see the module docs for why that is the correct trade for this check and where the sensitivity actually comes from.

Bounds are constants of the orbit class. None of them is derived from the series being validated.

Variants

MeoGnss

GNSS MEO: GLONASS (a ~ 25 510 km) through Galileo (a ~ 29 600 km), covering GPS, BeiDou MEO, NavIC MEO, and QZSS’s MEO-like arcs.

Geosynchronous

Geostationary and inclined-geosynchronous (a ~ 42 164 km), including BeiDou GEO/IGSO and QZSS.

Leo

Low earth orbit from a ~ 6 678 km (300 km altitude) upward.

Implementations

impl OrbitClass

pub fn max_earth_fixed_speed_m_s(self) -> f64

Physical earth-fixed speed bound for the class, meters per second.

Trait Implementations

impl Clone for OrbitClass

fn clone(&self) -> OrbitClass

Returns a duplicate of the value.

fn clone_from(&mut self, source: &Self)

Performs copy-assignment from source.

impl Copy for OrbitClass

impl Debug for OrbitClass

fn fmt(&self, f: &mut Formatter<'_>) -> Result

Formats the value using the given formatter.

impl Eq for OrbitClass

impl PartialEq for OrbitClass

fn eq(&self, other: &OrbitClass) -> bool

Equality operator ==.

fn ne(&self, other: &Rhs) -> bool

Inequality operator !=.

impl StructuralPartialEq for OrbitClass