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 25636U 99008C 23081.36213432 .00000872 00000-0 22631-3 0 9990
2 25636 96.4657 221.1824 0146081 126.4951 234.9805 14.45082936268581
| Epoch (UTC): | 22 March 2023 08:41:28 |
| Eccentricity: | 0.0146081 |
| inclination: | 96.4657° |
| perigee height: | 638 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 221.1824° |
| argument of perigee: | 126.4951° |
| revolutions per day: | 14.45082936 |
| mean anomaly at epoch: | 234.9805° |
| orbit number at epoch: | 26858 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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