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 40910U 15049M 22178.58562321 .00007698 00000-0 32806-3 0 9997
2 40910 97.4717 185.5892 0011180 305.6939 172.8604 15.23179222374720
| Epoch (UTC): | 27 June 2022 14:03:17 |
| Eccentricity: | 0.0011180 |
| inclination: | 97.4717° |
| perigee height: | 488 km |
| apogee height: | 504 km |
| right ascension of ascending node: | 185.5892° |
| argument of perigee: | 305.6939° |
| revolutions per day: | 15.23179222 |
| mean anomaly at epoch: | 172.8604° |
| orbit number at epoch: | 37472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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