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 29876U 99025FW 24279.43433139 .00002045 00000-0 96633-3 0 9992
2 29876 98.3915 347.6473 0061612 196.2457 226.8016 14.19783749917671
| Epoch (UTC): | 05 October 2024 10:25:26 |
| Eccentricity: | 0.0061612 |
| inclination: | 98.3915° |
| perigee height: | 782 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 347.6473° |
| argument of perigee: | 196.2457° |
| revolutions per day: | 14.19783749 |
| mean anomaly at epoch: | 226.8016° |
| orbit number at epoch: | 91767 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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