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 22178.42228867 .00021562 00000-0 60798-3 0 9990
2 40900 97.3998 196.4541 0006954 241.3191 226.3267 15.36410178376140
Epoch (UTC): | 27 June 2022 10:08:05 |
Eccentricity: | 0.0006954 |
inclination: | 97.3998° |
perigee height: | 452 km |
apogee height: | 461 km |
right ascension of ascending node: | 196.4541° |
argument of perigee: | 241.3191° |
revolutions per day: | 15.36410178 |
mean anomaly at epoch: | 226.3267° |
orbit number at epoch: | 37614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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