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 39770U 14029E 23265.67045685 .00032951 00000-0 22049-2 0 9990
2 39770 97.9955 36.1775 0005519 337.9918 22.1071 15.06844600506818
| Epoch (UTC): | 22 September 2023 16:05:27 |
| Eccentricity: | 0.0005519 |
| inclination: | 97.9955° |
| perigee height: | 542 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 36.1775° |
| argument of perigee: | 337.9918° |
| revolutions per day: | 15.06844600 |
| mean anomaly at epoch: | 22.1071° |
| orbit number at epoch: | 50681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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