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 40129U 14050B 23331.14614994 -.00000101 00000-0 00000-0 0 9999
2 40129 49.8781 310.2854 1604405 144.3468 227.5316 1.85520329 63176
| Epoch (UTC): | 27 November 2023 03:30:27 |
| Eccentricity: | 0.1604405 |
| inclination: | 49.8781° |
| perigee height: | 17110 km |
| apogee height: | 26088 km |
| right ascension of ascending node: | 310.2854° |
| argument of perigee: | 144.3468° |
| revolutions per day: | 1.85520329 |
| mean anomaly at epoch: | 227.5316° |
| orbit number at epoch: | 6317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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