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 22027.52324185 -.00000119 00000-0 -32952-3 0 9990
2 00050 47.2321 92.9911 0114101 281.0133 77.7840 12.20118632742140
| Epoch (UTC): | 27 January 2022 12:33:28 |
| Eccentricity: | 0.0114101 |
| inclination: | 47.2321° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 92.9911° |
| argument of perigee: | 281.0133° |
| revolutions per day: | 12.20118632 |
| mean anomaly at epoch: | 77.7840° |
| orbit number at epoch: | 74214 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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