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 40614U 15022B 23263.60578892 0.00000000 00000-0 00000-0 0 09
2 40614 0.0170 254.3626 0003615 150.4594 209.5406 1.00270000 02
| Epoch (UTC): | 20 September 2023 14:32:20 |
| Eccentricity: | 0.0003615 |
| inclination: | 0.0170° |
| perigee height: | 35771 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 254.3626° |
| argument of perigee: | 150.4594° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 209.5406° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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