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 39134U 13015E 22175.89085049 .00008804 00000-0 31589-3 0 9999
2 39134 64.8629 37.4805 0034901 278.5718 81.1460 15.28697156507999
| Epoch (UTC): | 24 June 2022 21:22:49 |
| Eccentricity: | 0.0034901 |
| inclination: | 64.8629° |
| perigee height: | 456 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 37.4805° |
| argument of perigee: | 278.5718° |
| revolutions per day: | 15.28697156 |
| mean anomaly at epoch: | 81.1460° |
| orbit number at epoch: | 50799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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