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 21019.84504410 .00000082 00000-0 16582-4 0 9992
2 06155 35.0049 65.4362 0037557 168.3809 191.7764 14.71638963564512
| Epoch (UTC): | 19 January 2021 20:16:51 |
| Eccentricity: | 0.0037557 |
| inclination: | 35.0049° |
| perigee height: | 629 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 65.4362° |
| argument of perigee: | 168.3809° |
| revolutions per day: | 14.71638963 |
| mean anomaly at epoch: | 191.7764° |
| orbit number at epoch: | 56451 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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