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 00050U 60009B 24357.42755769 -.00000043 00000-0 39728-3 0 9996
2 00050 47.2334 43.3030 0114004 200.4512 159.1691 12.20151360871556
| Epoch (UTC): | 22 December 2024 10:15:40 |
| Eccentricity: | 0.0114004 |
| inclination: | 47.2334° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 43.3030° |
| argument of perigee: | 200.4512° |
| revolutions per day: | 12.20151360 |
| mean anomaly at epoch: | 159.1691° |
| orbit number at epoch: | 87155 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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