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 26549U 00057E 19345.81557897 -.00000063 +00000-0 +10994-4 0 9997
2 26549 064.5497 191.4020 0058049 284.4868 074.9802 14.83611635038049
| Epoch (UTC): | 11 December 2019 19:34:26 |
| Eccentricity: | 0.0058049 |
| inclination: | 64.5497° |
| perigee height: | 577 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 191.4020° |
| argument of perigee: | 284.4868° |
| revolutions per day: | 14.83611635 |
| mean anomaly at epoch: | 74.9802° |
| orbit number at epoch: | 3804 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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