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 30566U 99025ALG 24358.05292708 .00004056 00000-0 22984-2 0 9992
2 30566 99.2435 31.1389 0068723 93.9856 296.5986 14.09431477913812
| Epoch (UTC): | 23 December 2024 01:16:12 |
| Eccentricity: | 0.0068723 |
| inclination: | 99.2435° |
| perigee height: | 811 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 31.1389° |
| argument of perigee: | 93.9856° |
| revolutions per day: | 14.09431477 |
| mean anomaly at epoch: | 296.5986° |
| orbit number at epoch: | 91381 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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