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 42766U 17036B 23083.63400276 .00051781 00000-0 15290-2 0 9997
2 42766 97.1682 117.0743 0012373 56.2879 303.9542 15.34717365319625
| Epoch (UTC): | 24 March 2023 15:12:57 |
| Eccentricity: | 0.0012373 |
| inclination: | 97.1682° |
| perigee height: | 453 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 117.0743° |
| argument of perigee: | 56.2879° |
| revolutions per day: | 15.34717365 |
| mean anomaly at epoch: | 303.9542° |
| orbit number at epoch: | 31962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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