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 35703U 93036APY 24355.82525056 .00009924 00000-0 11577-2 0 9998
2 35703 74.0461 33.1924 0075075 201.4153 158.3881 14.83245117613116
| Epoch (UTC): | 20 December 2024 19:48:21 |
| Eccentricity: | 0.0075075 |
| inclination: | 74.0461° |
| perigee height: | 566 km |
| apogee height: | 671 km |
| right ascension of ascending node: | 33.1924° |
| argument of perigee: | 201.4153° |
| revolutions per day: | 14.83245117 |
| mean anomaly at epoch: | 158.3881° |
| orbit number at epoch: | 61311 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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