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 22026.59760586 .00000081 00000-0 40239-4 0 9996
2 27386 98.1690 14.4755 0001177 86.8767 24.7371 14.38071361 43077
| Epoch (UTC): | 26 January 2022 14:20:33 |
| Eccentricity: | 0.0001177 |
| inclination: | 98.1690° |
| perigee height: | 764 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 14.4755° |
| argument of perigee: | 86.8767° |
| revolutions per day: | 14.38071361 |
| mean anomaly at epoch: | 24.7371° |
| orbit number at epoch: | 4307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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