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 25861U 99039B 23151.07826009 .00000501 00000-0 74566-4 0 9994
2 25861 98.1391 188.1829 0014132 296.6890 63.2873 14.79326333287011
Epoch (UTC): | 31 May 2023 01:52:41 |
Eccentricity: | 0.0014132 |
inclination: | 98.1391° |
perigee height: | 621 km |
apogee height: | 641 km |
right ascension of ascending node: | 188.1829° |
argument of perigee: | 296.6890° |
revolutions per day: | 14.79326333 |
mean anomaly at epoch: | 63.2873° |
orbit number at epoch: | 28701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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