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 23337.46239291 .00001189 00000-0 48054-3 0 9990
2 00020 33.3452 353.9883 1656426 139.4111 234.2570 11.57986463376956
| Epoch (UTC): | 03 December 2023 11:05:50 |
| Eccentricity: | 0.1656426 |
| inclination: | 33.3452° |
| perigee height: | 507 km |
| apogee height: | 3241 km |
| right ascension of ascending node: | 353.9883° |
| argument of perigee: | 139.4111° |
| revolutions per day: | 11.57986463 |
| mean anomaly at epoch: | 234.2570° |
| orbit number at epoch: | 37695 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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