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 24163.54141734 .14136259 24115-5 22659-3 0 9993
2 42793 97.0194 202.5662 0010261 237.3230 122.7085 16.47770263388951
| Epoch (UTC): | 11 June 2024 12:59:38 |
| Eccentricity: | 0.0010261 |
| inclination: | 97.0194° |
| perigee height: | 138 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 202.5662° |
| argument of perigee: | 237.3230° |
| revolutions per day: | 16.47770263 |
| mean anomaly at epoch: | 122.7085° |
| orbit number at epoch: | 38895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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