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 35498U 09036A 21025.68261156 -.00000004 00000-0 -10433-3 0 9992
2 35498 82.4867 233.7395 0007151 162.6419 197.4905 12.40823059523561
Epoch (UTC): | 25 January 2021 16:22:57 |
Eccentricity: | 0.0007151 |
inclination: | 82.4867° |
perigee height: | 1497 km |
apogee height: | 1509 km |
right ascension of ascending node: | 233.7395° |
argument of perigee: | 162.6419° |
revolutions per day: | 12.40823059 |
mean anomaly at epoch: | 197.4905° |
orbit number at epoch: | 52356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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