View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 30814U 99025AUY 23332.30762668 .00013326 00000-0 45886-2 0 9990
2 30814 99.0560 245.3333 0048805 294.2477 189.4766 14.35387112869616
| Epoch (UTC): | 28 November 2023 07:22:58 |
| Eccentricity: | 0.0048805 |
| inclination: | 99.0560° |
| perigee height: | 739 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 245.3333° |
| argument of perigee: | 294.2477° |
| revolutions per day: | 14.35387112 |
| mean anomaly at epoch: | 189.4766° |
| orbit number at epoch: | 86961 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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