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 52150U 22031A 24358.23803223 .00006355 00000-0 52615-3 0 9997
2 52150 97.8416 177.9952 0013519 179.4589 180.6650 14.99165539149284
| Epoch (UTC): | 23 December 2024 05:42:45 |
| Eccentricity: | 0.0013519 |
| inclination: | 97.8416° |
| perigee height: | 560 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 177.9952° |
| argument of perigee: | 179.4589° |
| revolutions per day: | 14.99165539 |
| mean anomaly at epoch: | 180.6650° |
| orbit number at epoch: | 14928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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