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 2680U 67014A 19345.75265358 -.00000039 +00000-0 +13054-4 0 9997
2 2680 039.4409 210.5802 0719442 197.1749 160.3410 13.38066771556890
| Epoch (UTC): | 11 December 2019 18:03:49 |
| Eccentricity: | 0.0719442 |
| inclination: | 39.4409° |
| perigee height: | 577 km |
| apogee height: | 1655 km |
| right ascension of ascending node: | 210.5802° |
| argument of perigee: | 197.1749° |
| revolutions per day: | 13.38066771 |
| mean anomaly at epoch: | 160.3410° |
| orbit number at epoch: | 55689 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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