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 23159.53312723 .00000620 00000-0 90561-4 0 9991
2 25861 98.1384 196.7429 0014020 266.7422 93.2185 14.79338325288136
Epoch (UTC): | 08 June 2023 12:47:42 |
Eccentricity: | 0.0014020 |
inclination: | 98.1384° |
perigee height: | 621 km |
apogee height: | 641 km |
right ascension of ascending node: | 196.7429° |
argument of perigee: | 266.7422° |
revolutions per day: | 14.79338325 |
mean anomaly at epoch: | 93.2185° |
orbit number at epoch: | 28813 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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