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 40967U 15058D 22180.22931330 .00001061 00000-0 12668-3 0 4068
2 40967 64.7758 36.2088 0194103 196.6635 162.8037 14.77446027 62407
Epoch (UTC): | 29 June 2022 05:30:12 |
Eccentricity: | 0.0194103 |
inclination: | 64.7758° |
perigee height: | 501 km |
apogee height: | 773 km |
right ascension of ascending node: | 36.2088° |
argument of perigee: | 196.6635° |
revolutions per day: | 14.77446027 |
mean anomaly at epoch: | 162.8037° |
orbit number at epoch: | 6240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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