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 40074U 14037F 22136.21838612 .00001799 00000-0 21651-3 0 9999
2 40074 98.3869 15.1966 0005474 42.6834 317.4809 14.85261107425283
| Epoch (UTC): | 16 May 2022 05:14:28 |
| Eccentricity: | 0.0005474 |
| inclination: | 98.3869° |
| perigee height: | 609 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 15.1966° |
| argument of perigee: | 42.6834° |
| revolutions per day: | 14.85261107 |
| mean anomaly at epoch: | 317.4809° |
| orbit number at epoch: | 42528 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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