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 21024.77516964 -.00000119 00000-0 -32344-3 0 9996
2 00050 47.2306 154.3622 0113599 265.0490 93.7322 12.20114461697242
| Epoch (UTC): | 24 January 2021 18:36:14 |
| Eccentricity: | 0.0113599 |
| inclination: | 47.2306° |
| perigee height: | 1501 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 154.3622° |
| argument of perigee: | 265.0490° |
| revolutions per day: | 12.20114461 |
| mean anomaly at epoch: | 93.7322° |
| orbit number at epoch: | 69724 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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