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 00051U 60009C 22027.51475954 -.00000032 00000-0 52528-3 0 9995
2 00051 47.2143 325.0171 0105387 113.6830 247.5058 12.18274672735909
| Epoch (UTC): | 27 January 2022 12:21:15 |
| Eccentricity: | 0.0105387 |
| inclination: | 47.2143° |
| perigee height: | 1516 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 325.0171° |
| argument of perigee: | 113.6830° |
| revolutions per day: | 12.18274672 |
| mean anomaly at epoch: | 247.5058° |
| orbit number at epoch: | 73590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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