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 32379U 07060B 22221.60869064 .00002929 00000-0 89377-3 0 9994
2 32379 60.8588 57.7418 5016597 177.4966 186.6713 5.53859752 61172
| Epoch (UTC): | 09 August 2022 14:36:30 |
| Eccentricity: | 0.5016597 |
| inclination: | 60.8588° |
| perigee height: | 346 km |
| apogee height: | 13885 km |
| right ascension of ascending node: | 57.7418° |
| argument of perigee: | 177.4966° |
| revolutions per day: | 5.53859752 |
| mean anomaly at epoch: | 186.6713° |
| orbit number at epoch: | 6117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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