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 19650U 88102B 21016.78560526 -.00000029 00000-0 96802-5 0 9991
2 19650 71.0005 141.3159 0015010 340.5166 19.5381 14.15800899661074
| Epoch (UTC): | 16 January 2021 18:51:16 |
| Eccentricity: | 0.0015010 |
| inclination: | 71.0005° |
| perigee height: | 829 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 141.3159° |
| argument of perigee: | 340.5166° |
| revolutions per day: | 14.15800899 |
| mean anomaly at epoch: | 19.5381° |
| orbit number at epoch: | 66107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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