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 22177.43588567 .00007945 00000-0 34286-3 0 9998
2 39136 64.8757 76.8735 0016756 296.0779 63.8625 15.23051328507284
| Epoch (UTC): | 26 June 2022 10:27:40 |
| Eccentricity: | 0.0016756 |
| inclination: | 64.8757° |
| perigee height: | 485 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 76.8735° |
| argument of perigee: | 296.0779° |
| revolutions per day: | 15.23051328 |
| mean anomaly at epoch: | 63.8625° |
| orbit number at epoch: | 50728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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