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 15755U 85042A 23338.46689782 .00000043 00000-0 41579-4 0 9998
2 15755 71.1127 67.9046 0036149 339.6232 20.3450 14.20639280996000
| Epoch (UTC): | 04 December 2023 11:12:19 |
| Eccentricity: | 0.0036149 |
| inclination: | 71.1127° |
| perigee height: | 797 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 67.9046° |
| argument of perigee: | 339.6232° |
| revolutions per day: | 14.20639280 |
| mean anomaly at epoch: | 20.3450° |
| orbit number at epoch: | 99600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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