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 16792U 86046B 23147.00695031 .00000428 00000-0 48654-4 0 9995
2 16792 82.4809 320.1992 0023627 350.7607 9.3170 14.83794300996522
| Epoch (UTC): | 27 May 2023 00:10:00 |
| Eccentricity: | 0.0023627 |
| inclination: | 82.4809° |
| perigee height: | 601 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 320.1992° |
| argument of perigee: | 350.7607° |
| revolutions per day: | 14.83794300 |
| mean anomaly at epoch: | 9.3170° |
| orbit number at epoch: | 99652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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