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 50466U 21131B 23031.58849904 .00000350 00000-0 12858-3 0 9990
2 50466 98.5626 113.5408 0004834 177.1391 182.9825 14.38650840 57713
| Epoch (UTC): | 31 January 2023 14:07:26 |
| Eccentricity: | 0.0004834 |
| inclination: | 98.5626° |
| perigee height: | 759 km |
| apogee height: | 766 km |
| right ascension of ascending node: | 113.5408° |
| argument of perigee: | 177.1391° |
| revolutions per day: | 14.38650840 |
| mean anomaly at epoch: | 182.9825° |
| orbit number at epoch: | 5771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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