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 40021U 14033M 22177.85773678 .00002553 00000-0 25149-3 0 9997
2 40021 98.0123 128.2292 0012991 16.9200 343.2449 14.92924892436101
Epoch (UTC): | 26 June 2022 20:35:08 |
Eccentricity: | 0.0012991 |
inclination: | 98.0123° |
perigee height: | 580 km |
apogee height: | 598 km |
right ascension of ascending node: | 128.2292° |
argument of perigee: | 16.9200° |
revolutions per day: | 14.92924892 |
mean anomaly at epoch: | 343.2449° |
orbit number at epoch: | 43610 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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