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 40907U 15049J 23081.30853991 .00018369 00000-0 72681-3 0 9995
2 40907 97.4962 88.6154 0013919 99.9626 25.3702 15.25418825415229
| Epoch (UTC): | 22 March 2023 07:24:17 |
| Eccentricity: | 0.0013919 |
| inclination: | 97.4962° |
| perigee height: | 480 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 88.6154° |
| argument of perigee: | 99.9626° |
| revolutions per day: | 15.25418825 |
| mean anomaly at epoch: | 25.3702° |
| orbit number at epoch: | 41522 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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