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 29252U 06029A 21066.21931468 .00000576 00000-0 37560-4 0 9999
2 29252 64.5219 161.9402 0032180 335.6208 24.3391 15.18505758808073
Epoch (UTC): | 07 March 2021 05:15:48 |
Eccentricity: | 0.0032180 |
inclination: | 64.5219° |
perigee height: | 488 km |
apogee height: | 532 km |
right ascension of ascending node: | 161.9402° |
argument of perigee: | 335.6208° |
revolutions per day: | 15.18505758 |
mean anomaly at epoch: | 24.3391° |
orbit number at epoch: | 80807 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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