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 26091U 00004J 23082.82109921 .00004389 00000-0 11160-2 0 9994
2 26091 100.2143 280.9801 0028933 148.5288 211.7639 14.51127678218563
| Epoch (UTC): | 23 March 2023 19:42:22 |
| Eccentricity: | 0.0028933 |
| inclination: | 100.2143° |
| perigee height: | 701 km |
| apogee height: | 742 km |
| right ascension of ascending node: | 280.9801° |
| argument of perigee: | 148.5288° |
| revolutions per day: | 14.51127678 |
| mean anomaly at epoch: | 211.7639° |
| orbit number at epoch: | 21856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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