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 40376U 15003A 22140.54050005 .00000691 00000-0 14267-3 0 9996
2 40376 98.1245 147.7719 0001002 88.7347 271.3970 14.63442338389903
| Epoch (UTC): | 20 May 2022 12:58:19 |
| Eccentricity: | 0.0001002 |
| inclination: | 98.1245° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 147.7719° |
| argument of perigee: | 88.7347° |
| revolutions per day: | 14.63442338 |
| mean anomaly at epoch: | 271.3970° |
| orbit number at epoch: | 38990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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