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 41604U 16040F 19340.88840985 +.00000311 +00000-0 +16663-4 0 9994
2 41604 097.3438 038.3325 0013477 139.4845 220.7397 15.21859581191939
| Epoch (UTC): | 06 December 2019 21:19:18 |
| Eccentricity: | 0.0013477 |
| inclination: | 97.3438° |
| perigee height: | 491 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 38.3325° |
| argument of perigee: | 139.4845° |
| revolutions per day: | 15.21859581 |
| mean anomaly at epoch: | 220.7397° |
| orbit number at epoch: | 19193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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