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 40057U 14034E 23090.46933365 .00007018 00000-0 90722-3 0 9990
2 40057 98.3733 280.0198 0010807 129.1523 231.0649 14.81212828471923
| Epoch (UTC): | 31 March 2023 11:15:50 |
| Eccentricity: | 0.0010807 |
| inclination: | 98.3733° |
| perigee height: | 618 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 280.0198° |
| argument of perigee: | 129.1523° |
| revolutions per day: | 14.81212828 |
| mean anomaly at epoch: | 231.0649° |
| orbit number at epoch: | 47192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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