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 19420U 88074B 19341.40946990 .00000049 00000-0 68597-4 0 9994
2 19420 89.9941 18.1017 0095364 28.2654 341.9546 13.42234737531995
| Epoch (UTC): | 07 December 2019 09:49:38 |
| Eccentricity: | 0.0095364 |
| inclination: | 89.9941° |
| perigee height: | 1029 km |
| apogee height: | 1172 km |
| right ascension of ascending node: | 18.1017° |
| argument of perigee: | 28.2654° |
| revolutions per day: | 13.42234737 |
| mean anomaly at epoch: | 341.9546° |
| orbit number at epoch: | 53199 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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