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 20978U 90105A 23337.57020990 .00000759 00000-0 25400-3 0 9996
2 20978 98.7379 10.1257 0072861 163.1977 197.1648 14.38836473729196
| Epoch (UTC): | 03 December 2023 13:41:06 |
| Eccentricity: | 0.0072861 |
| inclination: | 98.7379° |
| perigee height: | 710 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 10.1257° |
| argument of perigee: | 163.1977° |
| revolutions per day: | 14.38836473 |
| mean anomaly at epoch: | 197.1648° |
| orbit number at epoch: | 72919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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