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 22135.97658503 .00001221 00000-0 11204-3 0 9993
2 40014 98.1443 133.0626 0031674 142.6972 217.6460 14.96538917431280
| Epoch (UTC): | 15 May 2022 23:26:16 |
| Eccentricity: | 0.0031674 |
| inclination: | 98.1443° |
| perigee height: | 555 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 133.0626° |
| argument of perigee: | 142.6972° |
| revolutions per day: | 14.96538917 |
| mean anomaly at epoch: | 217.6460° |
| orbit number at epoch: | 43128 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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