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 23152.38741483 .00000189 00000-0 12350-3 0 9994
2 31793 70.9730 139.7980 0001619 265.5656 200.6116 14.14532627822205
| Epoch (UTC): | 01 June 2023 09:17:52 |
| Eccentricity: | 0.0001619 |
| inclination: | 70.9730° |
| perigee height: | 843 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 139.7980° |
| argument of perigee: | 265.5656° |
| revolutions per day: | 14.14532627 |
| mean anomaly at epoch: | 200.6116° |
| orbit number at epoch: | 82220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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