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 56630U 22151AFE 24355.73449752 .00002666 00000-0 14934-2 0 9994
2 56630 98.8284 353.2747 0055284 78.6817 282.0559 14.10731511 85247
| Epoch (UTC): | 20 December 2024 17:37:40 |
| Eccentricity: | 0.0055284 |
| inclination: | 98.8284° |
| perigee height: | 817 km |
| apogee height: | 897 km |
| right ascension of ascending node: | 353.2747° |
| argument of perigee: | 78.6817° |
| revolutions per day: | 14.10731511 |
| mean anomaly at epoch: | 282.0559° |
| orbit number at epoch: | 8524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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