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 23157.66359272 .00103019 00000-0 12233-2 0 9995
2 39134 64.8496 321.5824 0018191 258.9823 100.9278 15.60432315561729
| Epoch (UTC): | 06 June 2023 15:55:34 |
| Eccentricity: | 0.0018191 |
| inclination: | 64.8496° |
| perigee height: | 374 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 321.5824° |
| argument of perigee: | 258.9823° |
| revolutions per day: | 15.60432315 |
| mean anomaly at epoch: | 100.9278° |
| orbit number at epoch: | 56172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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