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 40931U 15052B 22277.17801041 .00001013 00000-0 51477-4 0 9995
2 40931 5.9961 113.4130 0013542 272.3153 87.5469 14.76872150379447
| Epoch (UTC): | 04 October 2022 04:16:20 |
| Eccentricity: | 0.0013542 |
| inclination: | 5.9961° |
| perigee height: | 630 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 113.4130° |
| argument of perigee: | 272.3153° |
| revolutions per day: | 14.76872150 |
| mean anomaly at epoch: | 87.5469° |
| orbit number at epoch: | 37944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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