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 41603U 16040E 19345.92149469 -.00000020 +00000-0 +21830-5 0 9993
2 41603 097.3390 040.0559 0014515 137.0032 035.8592 15.19773608192508
| Epoch (UTC): | 11 December 2019 22:06:57 |
| Eccentricity: | 0.0014515 |
| inclination: | 97.3390° |
| perigee height: | 496 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 40.0559° |
| argument of perigee: | 137.0032° |
| revolutions per day: | 15.19773608 |
| mean anomaly at epoch: | 35.8592° |
| orbit number at epoch: | 19250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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