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 31122U 07012F 19345.80099261 +.00000128 +00000-0 +34844-4 0 9994
2 31122 098.1409 293.2221 0078482 164.4566 195.9072 14.60959628673238
Epoch (UTC): | 11 December 2019 19:13:25 |
Eccentricity: | 0.0078482 |
inclination: | 98.1409° |
perigee height: | 634 km |
apogee height: | 745 km |
right ascension of ascending node: | 293.2221° |
argument of perigee: | 164.4566° |
revolutions per day: | 14.60959628 |
mean anomaly at epoch: | 195.9072° |
orbit number at epoch: | 67323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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