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 00020U 59007A 23343.32472560 .00000429 00000-0 16680-3 0 9996
2 00020 33.3466 333.0182 1656494 170.6368 192.9537 11.57993013377636
| Epoch (UTC): | 09 December 2023 07:47:36 |
| Eccentricity: | 0.1656494 |
| inclination: | 33.3466° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 333.0182° |
| argument of perigee: | 170.6368° |
| revolutions per day: | 11.57993013 |
| mean anomaly at epoch: | 192.9537° |
| orbit number at epoch: | 37763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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