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 22274.21669790 -.00000119 00000-0 -32805-3 0 9991
2 00050 47.2331 47.3270 0113447 296.4149 62.5035 12.20122179772267
| Epoch (UTC): | 01 October 2022 05:12:02 |
| Eccentricity: | 0.0113447 |
| inclination: | 47.2331° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 47.3270° |
| argument of perigee: | 296.4149° |
| revolutions per day: | 12.20122179 |
| mean anomaly at epoch: | 62.5035° |
| orbit number at epoch: | 77226 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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