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 15593U 85020B 23336.75110737 .00000949 00000-0 10778-3 0 9994
2 15593 82.5390 213.9640 0011887 156.5571 203.6190 14.85240045 73242
| Epoch (UTC): | 02 December 2023 18:01:35 |
| Eccentricity: | 0.0011887 |
| inclination: | 82.5390° |
| perigee height: | 604 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 213.9640° |
| argument of perigee: | 156.5571° |
| revolutions per day: | 14.85240045 |
| mean anomaly at epoch: | 203.6190° |
| orbit number at epoch: | 7324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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