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 00011U 59001A 23337.38066803 .00001411 00000-0 73273-3 0 9991
2 00011 32.8730 345.7927 1460159 193.0913 162.7452 11.87418789425109
| Epoch (UTC): | 03 December 2023 09:08:09 |
| Eccentricity: | 0.1460159 |
| inclination: | 32.8730° |
| perigee height: | 552 km |
| apogee height: | 2923 km |
| right ascension of ascending node: | 345.7927° |
| argument of perigee: | 193.0913° |
| revolutions per day: | 11.87418789 |
| mean anomaly at epoch: | 162.7452° |
| orbit number at epoch: | 42510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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