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 22139.52923137 .00000138 00000-0 12342-3 0 9993
2 14974 82.9370 245.0932 0045176 13.0038 357.5546 13.76937961909532
Epoch (UTC): | 19 May 2022 12:42:05 |
Eccentricity: | 0.0045176 |
inclination: | 82.9370° |
perigee height: | 941 km |
apogee height: | 1008 km |
right ascension of ascending node: | 245.0932° |
argument of perigee: | 13.0038° |
revolutions per day: | 13.76937961 |
mean anomaly at epoch: | 357.5546° |
orbit number at epoch: | 90953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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