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 22177.37800465 .00001619 00000-0 19482-3 0 9996
2 40074 98.3816 58.5144 0003045 270.1551 89.9307 14.85432608431399
| Epoch (UTC): | 26 June 2022 09:04:19 |
| Eccentricity: | 0.0003045 |
| inclination: | 98.3816° |
| perigee height: | 610 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 58.5144° |
| argument of perigee: | 270.1551° |
| revolutions per day: | 14.85432608 |
| mean anomaly at epoch: | 89.9307° |
| orbit number at epoch: | 43139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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