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 03598U 68110B 21016.43442341 .00000035 00000-0 12973-4 0 9990
2 03598 34.9926 142.9015 0048827 48.8622 311.6271 14.54504528736286
Epoch (UTC): | 16 January 2021 10:25:34 |
Eccentricity: | 0.0048827 |
inclination: | 34.9926° |
perigee height: | 676 km |
apogee height: | 745 km |
right ascension of ascending node: | 142.9015° |
argument of perigee: | 48.8622° |
revolutions per day: | 14.54504528 |
mean anomaly at epoch: | 311.6271° |
orbit number at epoch: | 73628 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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