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 40912U 15049P 22137.11537681 .00013213 00000-0 52479-3 0 9992
2 40912 97.4387 148.6818 0014816 58.5654 14.8632 15.25351506368975
| Epoch (UTC): | 17 May 2022 02:46:08 |
| Eccentricity: | 0.0014816 |
| inclination: | 97.4387° |
| perigee height: | 479 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 148.6818° |
| argument of perigee: | 58.5654° |
| revolutions per day: | 15.25351506 |
| mean anomaly at epoch: | 14.8632° |
| orbit number at epoch: | 36897 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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