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 40069U 14037A 22182.76084529 -.00000012 00000-0 13760-4 0 9995
2 40069 98.4303 199.9126 0004507 286.0964 73.9705 14.20711935413895
Epoch (UTC): | 01 July 2022 18:15:37 |
Eccentricity: | 0.0004507 |
inclination: | 98.4303° |
perigee height: | 820 km |
apogee height: | 826 km |
right ascension of ascending node: | 199.9126° |
argument of perigee: | 286.0964° |
revolutions per day: | 14.20711935 |
mean anomaly at epoch: | 73.9705° |
orbit number at epoch: | 41389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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