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 27665U 03005C 22147.81964649 .00000028 00000-0 44690-4 0 9994
2 27665 39.5758 275.3005 0007262 129.5646 1.9245 14.28613324 9067
| Epoch (UTC): | 27 May 2022 19:40:17 |
| Eccentricity: | 0.0007262 |
| inclination: | 39.5758° |
| perigee height: | 791 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 275.3005° |
| argument of perigee: | 129.5646° |
| revolutions per day: | 14.28613324 |
| mean anomaly at epoch: | 1.9245° |
| orbit number at epoch: | 906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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