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 59U 60013B 21109.15564405 .00000095 00000-0 10468-4 0 9994
2 59 28.2487 87.8705 0189048 332.0621 26.9885 13.52983742988545
Epoch (UTC): | 19 April 2021 03:44:07 |
Eccentricity: | 0.0189048 |
inclination: | 28.2487° |
perigee height: | 920 km |
apogee height: | 1202 km |
right ascension of ascending node: | 87.8705° |
argument of perigee: | 332.0621° |
revolutions per day: | 13.52983742 |
mean anomaly at epoch: | 26.9885° |
orbit number at epoch: | 98854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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