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 21796U 91081A 19340.90538537 +.00000045 +00000-0 +29935-4 0 9992
2 21796 082.9537 135.5955 0049727 160.6861 306.5938 13.75501494406600
Epoch (UTC): | 06 December 2019 21:43:45 |
Eccentricity: | 0.0049727 |
inclination: | 82.9537° |
perigee height: | 943 km |
apogee height: | 1016 km |
right ascension of ascending node: | 135.5955° |
argument of perigee: | 160.6861° |
revolutions per day: | 13.75501494 |
mean anomaly at epoch: | 306.5938° |
orbit number at epoch: | 40660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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