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 27845U 03031F 23088.73682694 .00001100 00000-0 50880-3 0 9995
2 27845 98.6729 97.9358 0009344 24.9885 335.1744 14.22857165 24325
| Epoch (UTC): | 29 March 2023 17:41:01 |
| Eccentricity: | 0.0009344 |
| inclination: | 98.6729° |
| perigee height: | 809 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 97.9358° |
| argument of perigee: | 24.9885° |
| revolutions per day: | 14.22857165 |
| mean anomaly at epoch: | 335.1744° |
| orbit number at epoch: | 2432 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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