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 04159U 69082AB 21016.63925828 -.00000039 00000-0 12512-4 0 9995
2 04159 69.9634 340.6656 0118653 260.7653 98.0004 13.72453955567307
| Epoch (UTC): | 16 January 2021 15:20:31 |
| Eccentricity: | 0.0118653 |
| inclination: | 69.9634° |
| perigee height: | 903 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 340.6656° |
| argument of perigee: | 260.7653° |
| revolutions per day: | 13.72453955 |
| mean anomaly at epoch: | 98.0004° |
| orbit number at epoch: | 56730 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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