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 39134U 13015E 22136.49501833 .00018532 00000-0 67914-3 0 9996
2 39134 64.8603 166.7114 0034268 286.8708 72.8666 15.27538899501971
| Epoch (UTC): | 16 May 2022 11:52:49 |
| Eccentricity: | 0.0034268 |
| inclination: | 64.8603° |
| perigee height: | 459 km |
| apogee height: | 506 km |
| right ascension of ascending node: | 166.7114° |
| argument of perigee: | 286.8708° |
| revolutions per day: | 15.27538899 |
| mean anomaly at epoch: | 72.8666° |
| orbit number at epoch: | 50197 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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