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 is defined by the following mean orbital elements,
1 42017U 17008BX 23199.44167461 .08967960 24048-5 93873-3 0 9998
2 42017 97.1901 272.9585 0015059 261.6732 98.2859 16.37376287358454
| Epoch (UTC): | 18 July 2023 10:36:00 |
| Eccentricity: | 0.0015059 |
| inclination: | 97.1901° |
| perigee height: | 163 km |
| apogee height: | 182 km |
| right ascension of ascending node: | 272.9585° |
| argument of perigee: | 261.6732° |
| revolutions per day: | 16.37376287 |
| mean anomaly at epoch: | 98.2859° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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