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 00046U 60007B 21024.56410689 -.00000016 00000-0 20039-4 0 9997
2 00046 66.6898 169.0714 0214556 324.7894 33.9191 14.49360594171159
| Epoch (UTC): | 24 January 2021 13:32:18 |
| Eccentricity: | 0.0214556 |
| inclination: | 66.6898° |
| perigee height: | 575 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 169.0714° |
| argument of perigee: | 324.7894° |
| revolutions per day: | 14.49360594 |
| mean anomaly at epoch: | 33.9191° |
| orbit number at epoch: | 17115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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