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 40042U 14033AJ 23341.42960168 .00006567 00000-0 56295-3 0 9994
2 40042 98.0304 294.1778 0014936 72.1891 288.0958 14.97798378513940
| Epoch (UTC): | 07 December 2023 10:18:37 |
| Eccentricity: | 0.0014936 |
| inclination: | 98.0304° |
| perigee height: | 563 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 294.1778° |
| argument of perigee: | 72.1891° |
| revolutions per day: | 14.97798378 |
| mean anomaly at epoch: | 288.0958° |
| orbit number at epoch: | 51394 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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