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 27511U 02040D 24281.99406986 .00000076 00000-0 26472-2 0 9996
2 27511 6.0273 322.7100 7159657 81.7805 322.5866 2.25658984181900
| Epoch (UTC): | 07 October 2024 23:51:27 |
| Eccentricity: | 0.7159657 |
| inclination: | 6.0273° |
| perigee height: | 595 km |
| apogee height: | 35753 km |
| right ascension of ascending node: | 322.7100° |
| argument of perigee: | 81.7805° |
| revolutions per day: | 2.25658984 |
| mean anomaly at epoch: | 322.5866° |
| orbit number at epoch: | 18190 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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