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 56639U 22151AFP 24356.52025571 .00000651 00000-0 27779-3 0 9994
2 56639 98.8059 19.3998 0041004 157.0944 203.2077 14.28083802 86863
| Epoch (UTC): | 21 December 2024 12:29:10 |
| Eccentricity: | 0.0041004 |
| inclination: | 98.8059° |
| perigee height: | 769 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 19.3998° |
| argument of perigee: | 157.0944° |
| revolutions per day: | 14.28083802 |
| mean anomaly at epoch: | 203.2077° |
| orbit number at epoch: | 8686 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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