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 28738U 05024B 21058.80960018 .00000589 00000-0 37618-4 0 9998
2 28738 97.3684 78.6908 0012540 28.6605 331.5312 15.12284668859995
Epoch (UTC): | 27 February 2021 19:25:49 |
Eccentricity: | 0.0012540 |
inclination: | 97.3684° |
perigee height: | 520 km |
apogee height: | 538 km |
right ascension of ascending node: | 78.6908° |
argument of perigee: | 28.6605° |
revolutions per day: | 15.12284668 |
mean anomaly at epoch: | 331.5312° |
orbit number at epoch: | 85999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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