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 18822U 88006A 23080.84151190 .00000406 00000-0 18165-3 0 9999
2 18822 98.3432 285.2966 0005772 332.6859 27.4018 14.27583780827393
| Epoch (UTC): | 21 March 2023 20:11:46 |
| Eccentricity: | 0.0005772 |
| inclination: | 98.3432° |
| perigee height: | 795 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 285.2966° |
| argument of perigee: | 332.6859° |
| revolutions per day: | 14.27583780 |
| mean anomaly at epoch: | 27.4018° |
| orbit number at epoch: | 82739 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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