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 26549U 00057E 23334.49987062 .00003664 00000-0 42273-3 0 9998
2 26549 64.5528 18.2405 0057046 259.1059 100.3626 14.86030683253435
| Epoch (UTC): | 30 November 2023 11:59:48 |
| Eccentricity: | 0.0057046 |
| inclination: | 64.5528° |
| perigee height: | 570 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 18.2405° |
| argument of perigee: | 259.1059° |
| revolutions per day: | 14.86030683 |
| mean anomaly at epoch: | 100.3626° |
| orbit number at epoch: | 25343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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