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 40958U 15057A 23271.70128275 .00001042 00000-0 16507-3 0 9990
2 40958 97.6951 300.4775 0016374 247.8909 112.0562 14.74100169428937
| Epoch (UTC): | 28 September 2023 16:49:50 |
| Eccentricity: | 0.0016374 |
| inclination: | 97.6951° |
| perigee height: | 636 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 300.4775° |
| argument of perigee: | 247.8909° |
| revolutions per day: | 14.74100169 |
| mean anomaly at epoch: | 112.0562° |
| orbit number at epoch: | 42893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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