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 23159.55652058 .00002315 00000-0 13824-3 0 9990
2 13068 81.1811 247.7724 0029583 303.8677 55.9734 15.10382126252331
Epoch (UTC): | 08 June 2023 13:21:23 |
Eccentricity: | 0.0029583 |
inclination: | 81.1811° |
perigee height: | 514 km |
apogee height: | 555 km |
right ascension of ascending node: | 247.7724° |
argument of perigee: | 303.8677° |
revolutions per day: | 15.10382126 |
mean anomaly at epoch: | 55.9734° |
orbit number at epoch: | 25233 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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