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 42778U 17036P 23085.87184274 .00024341 00000-0 71930-3 0 9991
2 42778 97.1687 122.8292 0009739 51.4948 308.7168 15.34886461320085
| Epoch (UTC): | 26 March 2023 20:55:27 |
| Eccentricity: | 0.0009739 |
| inclination: | 97.1687° |
| perigee height: | 454 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 122.8292° |
| argument of perigee: | 51.4948° |
| revolutions per day: | 15.34886461 |
| mean anomaly at epoch: | 308.7168° |
| orbit number at epoch: | 32008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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