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 35026U 93036AGP 24358.12150788 .00000547 00000-0 13276-3 0 9999
2 35026 74.0469 268.0767 0082911 112.2351 314.3307 14.53288753831054
| Epoch (UTC): | 23 December 2024 02:54:58 |
| Eccentricity: | 0.0082911 |
| inclination: | 74.0469° |
| perigee height: | 656 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 268.0767° |
| argument of perigee: | 112.2351° |
| revolutions per day: | 14.53288753 |
| mean anomaly at epoch: | 314.3307° |
| orbit number at epoch: | 83105 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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