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 11870U 80056B 23271.58094398 .00000356 00000-0 12766-3 0 9996
2 11870 74.0528 313.1343 0015369 51.9940 308.2599 14.37413804264389
| Epoch (UTC): | 28 September 2023 13:56:33 |
| Eccentricity: | 0.0015369 |
| inclination: | 74.0528° |
| perigee height: | 756 km |
| apogee height: | 778 km |
| right ascension of ascending node: | 313.1343° |
| argument of perigee: | 51.9940° |
| revolutions per day: | 14.37413804 |
| mean anomaly at epoch: | 308.2599° |
| orbit number at epoch: | 26438 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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