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 23157.09813163 .00000567 00000-0 83434-4 0 9995
2 25861 98.1386 194.2777 0014007 275.3974 84.5638 14.79334598287773
Epoch (UTC): | 06 June 2023 02:21:18 |
Eccentricity: | 0.0014007 |
inclination: | 98.1386° |
perigee height: | 621 km |
apogee height: | 641 km |
right ascension of ascending node: | 194.2777° |
argument of perigee: | 275.3974° |
revolutions per day: | 14.79334598 |
mean anomaly at epoch: | 84.5638° |
orbit number at epoch: | 28777 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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