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 00058U 60013A 21027.43183523 .00000084 00000-0 -13500-5 0 9991
2 00058 28.3287 38.3273 0165098 123.5896 238.0525 13.46325298968825
Epoch (UTC): | 27 January 2021 10:21:50 |
Eccentricity: | 0.0165098 |
inclination: | 28.3287° |
perigee height: | 962 km |
apogee height: | 1209 km |
right ascension of ascending node: | 38.3273° |
argument of perigee: | 123.5896° |
revolutions per day: | 13.46325298 |
mean anomaly at epoch: | 238.0525° |
orbit number at epoch: | 96882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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