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 17160U 86093B 23032.38194737 .00000036 00000-0 22107-4 0 9998
2 17160 82.9308 339.5921 0038721 178.9427 302.4992 13.74693458814954
| Epoch (UTC): | 01 February 2023 09:10:00 |
| Eccentricity: | 0.0038721 |
| inclination: | 82.9308° |
| perigee height: | 954 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 339.5921° |
| argument of perigee: | 178.9427° |
| revolutions per day: | 13.74693458 |
| mean anomaly at epoch: | 302.4992° |
| orbit number at epoch: | 81495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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