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 13114U 82025B 21016.70538381 .00000029 00000-0 12829-4 0 9999
2 13114 82.5383 240.7413 0015779 73.4774 349.0509 13.84680027961356
Epoch (UTC): | 16 January 2021 16:55:45 |
Eccentricity: | 0.0015779 |
inclination: | 82.5383° |
perigee height: | 936 km |
apogee height: | 959 km |
right ascension of ascending node: | 240.7413° |
argument of perigee: | 73.4774° |
revolutions per day: | 13.84680027 |
mean anomaly at epoch: | 349.0509° |
orbit number at epoch: | 96135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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