generated from ztimson/template
34 lines
1.1 KiB
JavaScript
34 lines
1.1 KiB
JavaScript
"use strict";
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Object.defineProperty(exports, "__esModule", {
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value: true
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});
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exports.SatRecError = void 0;
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var SatRecError;
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(function (SatRecError) {
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/**
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* No error, propagation for the last supplied date is successful
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*/
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SatRecError[SatRecError["None"] = 0] = "None";
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/**
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* Mean eccentricity is out of range 0 ≤ e < 1
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*/
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SatRecError[SatRecError["MeanEccentricityOutOfRange"] = 1] = "MeanEccentricityOutOfRange";
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/**
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* Mean motion has fallen below zero.
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*/
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SatRecError[SatRecError["MeanMotionBelowZero"] = 2] = "MeanMotionBelowZero";
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/**
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* Perturbed eccentricity is out of range 0 ≤ e < 1
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*/
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SatRecError[SatRecError["PerturbedEccentricityOutOfRange"] = 3] = "PerturbedEccentricityOutOfRange";
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/**
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* Length of the orbit’s semi-latus rectum has fallen below zero.
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*/
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SatRecError[SatRecError["SemiLatusRectumBelowZero"] = 4] = "SemiLatusRectumBelowZero";
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// 5 is not used
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/**
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* Orbit has decayed: the computed position is underground.
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*/
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SatRecError[SatRecError["Decayed"] = 6] = "Decayed";
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})(SatRecError || (exports.SatRecError = SatRecError = {})); |