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 38707U 12039A 24323.81578493 .08695980 26821-5 76758-3 0 9994
2 38707 97.4797 272.4019 0006631 150.5746 270.1213 16.39248839685412
| Epoch (UTC): | 18 November 2024 19:34:43 |
| Eccentricity: | 0.0006631 |
| inclination: | 97.4797° |
| perigee height: | 163 km |
| apogee height: | 172 km |
| right ascension of ascending node: | 272.4019° |
| argument of perigee: | 150.5746° |
| revolutions per day: | 16.39248839 |
| mean anomaly at epoch: | 270.1213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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