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 22175.75169282 .00001944 00000-0 26960-3 0 9999
2 40057 98.3658 348.5917 0009547 310.8619 49.1760 14.79169426430550
| Epoch (UTC): | 24 June 2022 18:02:26 |
| Eccentricity: | 0.0009547 |
| inclination: | 98.3658° |
| perigee height: | 625 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 348.5917° |
| argument of perigee: | 310.8619° |
| revolutions per day: | 14.79169426 |
| mean anomaly at epoch: | 49.1760° |
| orbit number at epoch: | 43055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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