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 22179.55425701 .00007352 00000-0 26453-3 0 9990
2 39134 64.8622 25.4533 0035067 277.6743 82.0407 15.28772891508553
| Epoch (UTC): | 28 June 2022 13:18:07 |
| Eccentricity: | 0.0035067 |
| inclination: | 64.8622° |
| perigee height: | 455 km |
| apogee height: | 503 km |
| right ascension of ascending node: | 25.4533° |
| argument of perigee: | 277.6743° |
| revolutions per day: | 15.28772891 |
| mean anomaly at epoch: | 82.0407° |
| orbit number at epoch: | 50855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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