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 22180.78460965 .00004260 00000-0 18783-3 0 9992
2 39136 64.8756 65.9796 0017122 296.2202 63.7166 15.23091749507796
| Epoch (UTC): | 29 June 2022 18:49:50 |
| Eccentricity: | 0.0017122 |
| inclination: | 64.8756° |
| perigee height: | 485 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 65.9796° |
| argument of perigee: | 296.2202° |
| revolutions per day: | 15.23091749 |
| mean anomaly at epoch: | 63.7166° |
| orbit number at epoch: | 50779 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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