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 26906U 01040B 24317.97484727 .00000861 00000-0 58566-3 0 9991
2 26906 63.4287 218.7147 0579970 340.3288 17.6164 13.44750639 25239
Epoch (UTC): | 12 November 2024 23:23:46 |
Eccentricity: | 0.0579970 |
inclination: | 63.4287° |
perigee height: | 658 km |
apogee height: | 1525 km |
right ascension of ascending node: | 218.7147° |
argument of perigee: | 340.3288° |
revolutions per day: | 13.44750639 |
mean anomaly at epoch: | 17.6164° |
orbit number at epoch: | 2523 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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