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 27848U 03031J 23082.99620991 .00000663 00000-0 31840-3 0 9990
2 27848 98.6849 91.9417 0010299 33.6330 326.5499 14.22214474 23447
| Epoch (UTC): | 23 March 2023 23:54:32 |
| Eccentricity: | 0.0010299 |
| inclination: | 98.6849° |
| perigee height: | 810 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 91.9417° |
| argument of perigee: | 33.6330° |
| revolutions per day: | 14.22214474 |
| mean anomaly at epoch: | 326.5499° |
| orbit number at epoch: | 2344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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