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 13068U 82013B 23151.14284177 .00001950 00000-0 11624-3 0 9990
2 13068 81.1829 257.4510 0030215 331.1907 28.7648 15.10346254251068
Epoch (UTC): | 31 May 2023 03:25:41 |
Eccentricity: | 0.0030215 |
inclination: | 81.1829° |
perigee height: | 514 km |
apogee height: | 556 km |
right ascension of ascending node: | 257.4510° |
argument of perigee: | 331.1907° |
revolutions per day: | 15.10346254 |
mean anomaly at epoch: | 28.7648° |
orbit number at epoch: | 25106 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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