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 26064U 00004D 23081.09979243 .00000213 00000-0 91979-4 0 9994
2 26064 100.2039 137.1355 0037988 154.4640 205.8428 14.36411916213101
Epoch (UTC): | 22 March 2023 02:23:42 |
Eccentricity: | 0.0037988 |
inclination: | 100.2039° |
perigee height: | 743 km |
apogee height: | 797 km |
right ascension of ascending node: | 137.1355° |
argument of perigee: | 154.4640° |
revolutions per day: | 14.36411916 |
mean anomaly at epoch: | 205.8428° |
orbit number at epoch: | 21310 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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