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 40908U 15049K 22135.76121766 .00003081 00000-0 16540-3 0 9990
2 40908 97.5163 136.6740 0016945 126.2741 47.9603 15.15568724367536
| Epoch (UTC): | 15 May 2022 18:16:09 |
| Eccentricity: | 0.0016945 |
| inclination: | 97.5163° |
| perigee height: | 507 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 136.6740° |
| argument of perigee: | 126.2741° |
| revolutions per day: | 15.15568724 |
| mean anomaly at epoch: | 47.9603° |
| orbit number at epoch: | 36753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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