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 58U 60013A 23027.13402887 .00000130 00000-0 72425-4 0 9998
2 58 28.3276 296.3142 0164852 44.9838 316.3934 13.46343554 67765
Epoch (UTC): | 27 January 2023 03:13:00 |
Eccentricity: | 0.0164852 |
inclination: | 28.3276° |
perigee height: | 963 km |
apogee height: | 1209 km |
right ascension of ascending node: | 296.3142° |
argument of perigee: | 44.9838° |
revolutions per day: | 13.46343554 |
mean anomaly at epoch: | 316.3934° |
orbit number at epoch: | 6776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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