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 31114U 07010B 22139.72402529 .00000238 00000-0 12942-3 0 9990
2 31114 98.2392 314.8426 0060131 22.9128 337.4712 14.19426439782498
Epoch (UTC): | 19 May 2022 17:22:35 |
Eccentricity: | 0.0060131 |
inclination: | 98.2392° |
perigee height: | 784 km |
apogee height: | 870 km |
right ascension of ascending node: | 314.8426° |
argument of perigee: | 22.9128° |
revolutions per day: | 14.19426439 |
mean anomaly at epoch: | 337.4712° |
orbit number at epoch: | 78249 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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