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 22228.57416785 .00006801 00000-0 28794-3 0 9999
2 39136 64.8729 270.4239 0020486 296.7920 63.1114 15.23795369515559
| Epoch (UTC): | 16 August 2022 13:46:48 |
| Eccentricity: | 0.0020486 |
| inclination: | 64.8729° |
| perigee height: | 480 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 270.4239° |
| argument of perigee: | 296.7920° |
| revolutions per day: | 15.23795369 |
| mean anomaly at epoch: | 63.1114° |
| orbit number at epoch: | 51555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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