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 60749U 24153E 24358.46907093 .00027643 00000-0 14228-2 0 9992
2 60749 97.6220 115.9051 0013551 249.2535 110.7246 15.16309059 17582
| Epoch (UTC): | 23 December 2024 11:15:27 |
| Eccentricity: | 0.0013551 |
| inclination: | 97.6220° |
| perigee height: | 507 km |
| apogee height: | 526 km |
| right ascension of ascending node: | 115.9051° |
| argument of perigee: | 249.2535° |
| revolutions per day: | 15.16309059 |
| mean anomaly at epoch: | 110.7246° |
| orbit number at epoch: | 1758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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