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 06155U 72065B 21015.57087187 .00000093 00000-0 18303-4 0 9990
2 06155 35.0043 90.2444 0037214 132.4244 227.9611 14.71638106563889
| Epoch (UTC): | 15 January 2021 13:42:03 |
| Eccentricity: | 0.0037214 |
| inclination: | 35.0043° |
| perigee height: | 629 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 90.2444° |
| argument of perigee: | 132.4244° |
| revolutions per day: | 14.71638106 |
| mean anomaly at epoch: | 227.9611° |
| orbit number at epoch: | 56388 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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