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 28895U 05043F 24315.33919687 .00009095 00000-0 15457-2 0 9992
2 28895 98.2214 91.6981 0014295 255.1196 104.8426 14.69299003 15907
Epoch (UTC): | 10 November 2024 08:08:26 |
Eccentricity: | 0.0014295 |
inclination: | 98.2214° |
perigee height: | 653 km |
apogee height: | 673 km |
right ascension of ascending node: | 91.6981° |
argument of perigee: | 255.1196° |
revolutions per day: | 14.69299003 |
mean anomaly at epoch: | 104.8426° |
orbit number at epoch: | 1590 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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