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 50U 60009B 22022.60901690 -.00000034 00000-0 47549-3 0 9999
2 50 47.2316 108.2426 0114031 266.3976 92.3767 12.20118442741991
| Epoch (UTC): | 22 January 2022 14:36:59 |
| Eccentricity: | 0.0114031 |
| inclination: | 47.2316° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 108.2426° |
| argument of perigee: | 266.3976° |
| revolutions per day: | 12.20118442 |
| mean anomaly at epoch: | 92.3767° |
| orbit number at epoch: | 74199 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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