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 20491U 90013D 24276.32636393 .00000165 00000-0 37097-3 0 9996
2 20491 99.0249 305.5449 0468202 179.7569 180.3854 13.03680919647867
| Epoch (UTC): | 02 October 2024 07:49:57 |
| Eccentricity: | 0.0468202 |
| inclination: | 99.0249° |
| perigee height: | 890 km |
| apogee height: | 1605 km |
| right ascension of ascending node: | 305.5449° |
| argument of perigee: | 179.7569° |
| revolutions per day: | 13.03680919 |
| mean anomaly at epoch: | 180.3854° |
| orbit number at epoch: | 64786 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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