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 21809U 91076E 18344.49629886 0.00000050 00000-0 12557-4 0 07
2 21809 63.3416 138.7405 0795000 28.5609 331.4391 13.41447495 00
| Epoch (UTC): | 10 December 2018 11:54:40 |
| Eccentricity: | 0.0795000 |
| inclination: | 63.3416° |
| perigee height: | 509 km |
| apogee height: | 1699 km |
| right ascension of ascending node: | 138.7405° |
| argument of perigee: | 28.5609° |
| revolutions per day: | 13.41447495 |
| mean anomaly at epoch: | 331.4391° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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