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 22142.45241315 .00000306 00000-0 11449-3 0 9994
2 27386 98.1819 124.7813 0001321 86.2071 72.8260 14.38122730 59720
| Epoch (UTC): | 22 May 2022 10:51:28 |
| Eccentricity: | 0.0001321 |
| inclination: | 98.1819° |
| perigee height: | 764 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 124.7813° |
| argument of perigee: | 86.2071° |
| revolutions per day: | 14.38122730 |
| mean anomaly at epoch: | 72.8260° |
| orbit number at epoch: | 5972 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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