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 01328U 65032A 21023.54022089 -.00000049 00000-0 52356-4 0 9997
2 01328 41.1830 167.7354 0259019 135.7811 226.3956 13.38641727724220
Epoch (UTC): | 23 January 2021 12:57:55 |
Eccentricity: | 0.0259019 |
inclination: | 41.1830° |
perigee height: | 920 km |
apogee height: | 1308 km |
right ascension of ascending node: | 167.7354° |
argument of perigee: | 135.7811° |
revolutions per day: | 13.38641727 |
mean anomaly at epoch: | 226.3956° |
orbit number at epoch: | 72422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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