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 22146.52914258 -.00000079 00000-0 47666-4 0 9991
2 00050 47.2322 83.6295 0114249 276.2671 82.5116 12.20121571756678
| Epoch (UTC): | 26 May 2022 12:41:57 |
| Eccentricity: | 0.0114249 |
| inclination: | 47.2322° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 83.6295° |
| argument of perigee: | 276.2671° |
| revolutions per day: | 12.20121571 |
| mean anomaly at epoch: | 82.5116° |
| orbit number at epoch: | 75667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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