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 23332.10898897 .00015389 00000-0 68422-3 0 9996
2 42759 43.0148 282.0895 0009696 91.1563 269.0398 15.21266121356567
| Epoch (UTC): | 28 November 2023 02:36:56 |
| Eccentricity: | 0.0009696 |
| inclination: | 43.0148° |
| perigee height: | 495 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 282.0895° |
| argument of perigee: | 91.1563° |
| revolutions per day: | 15.21266121 |
| mean anomaly at epoch: | 269.0398° |
| orbit number at epoch: | 35656 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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