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 31793U 07029B 23147.21937895 -.00000011 00000-0 18981-4 0 9996
2 31793 70.9725 150.6567 0001734 264.2855 172.4608 14.14531383821565
| Epoch (UTC): | 27 May 2023 05:15:54 |
| Eccentricity: | 0.0001734 |
| inclination: | 70.9725° |
| perigee height: | 842 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 150.6567° |
| argument of perigee: | 264.2855° |
| revolutions per day: | 14.14531383 |
| mean anomaly at epoch: | 172.4608° |
| orbit number at epoch: | 82156 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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