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 20625U 90046B 19343.58875819 +.00000211 +00000-0 +13408-3 0 9998
2 20625 070.9999 048.8176 0014295 180.7411 179.3693 14.14646361525621
| Epoch (UTC): | 09 December 2019 14:07:48 |
| Eccentricity: | 0.0014295 |
| inclination: | 70.9999° |
| perigee height: | 833 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 48.8176° |
| argument of perigee: | 180.7411° |
| revolutions per day: | 14.14646361 |
| mean anomaly at epoch: | 179.3693° |
| orbit number at epoch: | 52562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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