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 45094C 20006BC 21020.12119515 -.00005264 00000-0 -35277-3 0 201
2 45094 53.0600 21.8622 0001520 57.6426 33.4373 15.06398618 18
Epoch (UTC): | 20 January 2021 02:54:31 |
Eccentricity: | 0.0001520 |
inclination: | 53.0600° |
perigee height: | 546 km |
apogee height: | 548 km |
right ascension of ascending node: | 21.8622° |
argument of perigee: | 57.6426° |
revolutions per day: | 15.06398618 |
mean anomaly at epoch: | 33.4373° |
orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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