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 23087.18130163 .00098155 00000-0 13776-2 0 9997
2 42017 97.2229 156.3442 0002492 269.2445 90.8525 15.56395033340782
| Epoch (UTC): | 28 March 2023 04:21:04 |
| Eccentricity: | 0.0002492 |
| inclination: | 97.2229° |
| perigee height: | 396 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 156.3442° |
| argument of perigee: | 269.2445° |
| revolutions per day: | 15.56395033 |
| mean anomaly at epoch: | 90.8525° |
| orbit number at epoch: | 34078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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