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 42783U 17036U 23083.55050492 .00051924 00000-0 14783-2 0 9993
2 42783 97.1631 120.2944 0009746 60.2291 299.9922 15.35892811319784
| Epoch (UTC): | 24 March 2023 13:12:43 |
| Eccentricity: | 0.0009746 |
| inclination: | 97.1631° |
| perigee height: | 451 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 120.2944° |
| argument of perigee: | 60.2291° |
| revolutions per day: | 15.35892811 |
| mean anomaly at epoch: | 299.9922° |
| orbit number at epoch: | 31978 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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