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 22145.30058898 -.00000051 00000-0 31786-3 0 9990
2 00050 47.2319 87.4424 0114253 272.6152 86.1564 12.20121548756524
| Epoch (UTC): | 25 May 2022 07:12:50 |
| Eccentricity: | 0.0114253 |
| inclination: | 47.2319° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 87.4424° |
| argument of perigee: | 272.6152° |
| revolutions per day: | 12.20121548 |
| mean anomaly at epoch: | 86.1564° |
| orbit number at epoch: | 75652 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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