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 29784U 99025CA 24357.72835047 .00002378 00000-0 93606-3 0 9999
2 29784 98.9517 260.8139 0060336 249.4161 135.2152 14.29210689932864
| Epoch (UTC): | 22 December 2024 17:28:49 |
| Eccentricity: | 0.0060336 |
| inclination: | 98.9517° |
| perigee height: | 751 km |
| apogee height: | 837 km |
| right ascension of ascending node: | 260.8139° |
| argument of perigee: | 249.4161° |
| revolutions per day: | 14.29210689 |
| mean anomaly at epoch: | 135.2152° |
| orbit number at epoch: | 93286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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