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 40910U 15049M 22176.80452061 .00008520 00000-0 36297-3 0 9992
2 40910 97.4722 183.8175 0011294 313.3774 124.9441 15.23155710374453
Epoch (UTC): | 25 June 2022 19:18:30 |
Eccentricity: | 0.0011294 |
inclination: | 97.4722° |
perigee height: | 488 km |
apogee height: | 504 km |
right ascension of ascending node: | 183.8175° |
argument of perigee: | 313.3774° |
revolutions per day: | 15.23155710 |
mean anomaly at epoch: | 124.9441° |
orbit number at epoch: | 37445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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