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 42786U 17036X 23083.66696007 .00053499 00000-0 15067-2 0 9991
2 42786 97.1629 120.4981 0009675 60.3173 299.9034 15.36225789319798
| Epoch (UTC): | 24 March 2023 16:00:25 |
| Eccentricity: | 0.0009675 |
| inclination: | 97.1629° |
| perigee height: | 450 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 120.4981° |
| argument of perigee: | 60.3173° |
| revolutions per day: | 15.36225789 |
| mean anomaly at epoch: | 299.9034° |
| orbit number at epoch: | 31979 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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