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 36520U 10017B 24358.21725721 .00000113 00000-0 10588-3 0 9994
2 36520 82.9602 278.1349 0026246 168.2657 303.0378 13.72997603734537
| Epoch (UTC): | 23 December 2024 05:12:51 |
| Eccentricity: | 0.0026246 |
| inclination: | 82.9602° |
| perigee height: | 969 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 278.1349° |
| argument of perigee: | 168.2657° |
| revolutions per day: | 13.72997603 |
| mean anomaly at epoch: | 303.0378° |
| orbit number at epoch: | 73453 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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