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 39136U 13015G 22179.86535990 .00004947 00000-0 21669-3 0 9999
2 39136 64.8757 68.9703 0017020 295.9704 63.9671 15.23083307508131
| Epoch (UTC): | 28 June 2022 20:46:07 |
| Eccentricity: | 0.0017020 |
| inclination: | 64.8757° |
| perigee height: | 485 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 68.9703° |
| argument of perigee: | 295.9704° |
| revolutions per day: | 15.23083307 |
| mean anomaly at epoch: | 63.9671° |
| orbit number at epoch: | 50813 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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