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 40014U 14033E 22136.24403177 .00001350 00000-0 12321-3 0 9993
2 40014 98.1442 133.3416 0031500 142.0150 218.3303 14.96540548431321
| Epoch (UTC): | 16 May 2022 05:51:24 |
| Eccentricity: | 0.0031500 |
| inclination: | 98.1442° |
| perigee height: | 555 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 133.3416° |
| argument of perigee: | 142.0150° |
| revolutions per day: | 14.96540548 |
| mean anomaly at epoch: | 218.3303° |
| orbit number at epoch: | 43132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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