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 23150.41642431 .00000115 00000-0 84914-4 0 9994
2 31793 70.9726 143.9393 0001659 264.6710 247.5859 14.14531807821921
| Epoch (UTC): | 30 May 2023 09:59:39 |
| Eccentricity: | 0.0001659 |
| inclination: | 70.9726° |
| perigee height: | 843 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 143.9393° |
| argument of perigee: | 264.6710° |
| revolutions per day: | 14.14531807 |
| mean anomaly at epoch: | 247.5859° |
| orbit number at epoch: | 82192 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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