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 50496U 21132AD 23339.53423885 .00000097 00000-0 21440-3 0 9991
2 50496 87.9156 159.3966 0001303 69.4395 290.6877 13.18688795 99759
| Epoch (UTC): | 05 December 2023 12:49:18 |
| Eccentricity: | 0.0001303 |
| inclination: | 87.9156° |
| perigee height: | 1189 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 159.3966° |
| argument of perigee: | 69.4395° |
| revolutions per day: | 13.18688795 |
| mean anomaly at epoch: | 290.6877° |
| orbit number at epoch: | 9975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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