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 14974U 84046B 22148.18675395 .00000055 00000-0 39897-4 0 9998
2 14974 82.9372 238.6544 0044629 348.8351 72.6425 13.76938780910724
Epoch (UTC): | 28 May 2022 04:28:55 |
Eccentricity: | 0.0044629 |
inclination: | 82.9372° |
perigee height: | 942 km |
apogee height: | 1007 km |
right ascension of ascending node: | 238.6544° |
argument of perigee: | 348.8351° |
revolutions per day: | 13.76938780 |
mean anomaly at epoch: | 72.6425° |
orbit number at epoch: | 91072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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