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 27386U 02009A 22181.54422701 .00000033 00000-0 24414-4 0 9991
2 27386 98.1836 162.0380 0001336 90.4854 19.6065 14.38135248 65340
| Epoch (UTC): | 30 June 2022 13:03:41 |
| Eccentricity: | 0.0001336 |
| inclination: | 98.1836° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 162.0380° |
| argument of perigee: | 90.4854° |
| revolutions per day: | 14.38135248 |
| mean anomaly at epoch: | 19.6065° |
| orbit number at epoch: | 6534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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