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 42759U 17034B 23339.13380295 .00011938 00000-0 52968-3 0 9998
2 42759 43.0131 242.7982 0010392 142.7065 217.4508 15.21505426357637
| Epoch (UTC): | 05 December 2023 03:12:40 |
| Eccentricity: | 0.0010392 |
| inclination: | 43.0131° |
| perigee height: | 494 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 242.7982° |
| argument of perigee: | 142.7065° |
| revolutions per day: | 15.21505426 |
| mean anomaly at epoch: | 217.4508° |
| orbit number at epoch: | 35763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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