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 39679U 14021B 23159.08003672 .00005844 00000-0 26062-3 0 9998
2 39679 51.6116 95.5001 0154329 118.1094 243.5575 15.12851229502862
| Epoch (UTC): | 08 June 2023 01:55:15 |
| Eccentricity: | 0.0154329 |
| inclination: | 51.6116° |
| perigee height: | 421 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 95.5001° |
| argument of perigee: | 118.1094° |
| revolutions per day: | 15.12851229 |
| mean anomaly at epoch: | 243.5575° |
| orbit number at epoch: | 50286 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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