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 22182.88573362 .00003566 00000-0 15860-3 0 9992
2 39136 64.8750 59.1446 0017184 296.2645 63.6717 15.23108571508116
| Epoch (UTC): | 01 July 2022 21:15:27 |
| Eccentricity: | 0.0017184 |
| inclination: | 64.8750° |
| perigee height: | 484 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 59.1446° |
| argument of perigee: | 296.2645° |
| revolutions per day: | 15.23108571 |
| mean anomaly at epoch: | 63.6717° |
| orbit number at epoch: | 50811 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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