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 42017U 17008BX 23089.17412134 .00121914 00000-0 16771-2 0 9997
2 42017 97.2226 158.3615 0002756 261.8792 98.2151 15.56851929341092
| Epoch (UTC): | 30 March 2023 04:10:44 |
| Eccentricity: | 0.0002756 |
| inclination: | 97.2226° |
| perigee height: | 395 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 158.3615° |
| argument of perigee: | 261.8792° |
| revolutions per day: | 15.56851929 |
| mean anomaly at epoch: | 98.2151° |
| orbit number at epoch: | 34109 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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