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 42793U 17036AE 23083.64136820 .00046467 00000-0 13693-2 0 9999
2 42793 97.1616 120.7029 0008794 60.7330 299.4792 15.34846003319914
| Epoch (UTC): | 24 March 2023 15:23:34 |
| Eccentricity: | 0.0008794 |
| inclination: | 97.1616° |
| perigee height: | 455 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 120.7029° |
| argument of perigee: | 60.7330° |
| revolutions per day: | 15.34846003 |
| mean anomaly at epoch: | 299.4792° |
| orbit number at epoch: | 31991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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