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 21058.44807223 .00000666 00000-0 41903-4 0 9992
2 29252 64.5219 187.3720 0030818 335.8238 24.1436 15.18492317806813
Epoch (UTC): | 27 February 2021 10:45:13 |
Eccentricity: | 0.0030818 |
inclination: | 64.5219° |
perigee height: | 489 km |
apogee height: | 531 km |
right ascension of ascending node: | 187.3720° |
argument of perigee: | 335.8238° |
revolutions per day: | 15.18492317 |
mean anomaly at epoch: | 24.1436° |
orbit number at epoch: | 80681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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