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 20888U 90081AY 24357.49124994 .00004789 00000-0 16972-2 0 9992
2 20888 99.2253 180.5832 0187614 355.8260 4.1345 14.25649690749891
| Epoch (UTC): | 22 December 2024 11:47:23 |
| Eccentricity: | 0.0187614 |
| inclination: | 99.2253° |
| perigee height: | 671 km |
| apogee height: | 941 km |
| right ascension of ascending node: | 180.5832° |
| argument of perigee: | 355.8260° |
| revolutions per day: | 14.25649690 |
| mean anomaly at epoch: | 4.1345° |
| orbit number at epoch: | 74989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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