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 00047U 60007C 21100.66853734 -.00000026 00000-0 19106-4 0 9990
2 00047 66.6653 80.2578 0219846 85.6265 276.9922 14.42142118177535
| Epoch (UTC): | 10 April 2021 16:02:41 |
| Eccentricity: | 0.0219846 |
| inclination: | 66.6653° |
| perigee height: | 594 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 80.2578° |
| argument of perigee: | 85.6265° |
| revolutions per day: | 14.42142118 |
| mean anomaly at epoch: | 276.9922° |
| orbit number at epoch: | 17753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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