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 40900U 15049B 22177.95862652 .00021895 00000-0 61773-3 0 9996
2 40900 97.4001 195.9874 0006725 244.2734 180.5019 15.36391718376076
| Epoch (UTC): | 26 June 2022 23:00:25 |
| Eccentricity: | 0.0006725 |
| inclination: | 97.4001° |
| perigee height: | 452 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 195.9874° |
| argument of perigee: | 244.2734° |
| revolutions per day: | 15.36391718 |
| mean anomaly at epoch: | 180.5019° |
| orbit number at epoch: | 37607 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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