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 25338U 98030A 23081.80085253 .00000288 00000-0 13832-3 0 9994
2 25338 98.6164 112.2964 0010060 199.8934 160.1855 14.26272883292947
Epoch (UTC): | 22 March 2023 19:13:13 |
Eccentricity: | 0.0010060 |
inclination: | 98.6164° |
perigee height: | 797 km |
apogee height: | 811 km |
right ascension of ascending node: | 112.2964° |
argument of perigee: | 199.8934° |
revolutions per day: | 14.26272883 |
mean anomaly at epoch: | 160.1855° |
orbit number at epoch: | 29294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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