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 28097U 03054C 24224.83028283 0.00000500 00000-0 38876-3 0 09
2 28097 63.3883 118.0766 0532885 3.9106 356.0894 13.41016672 04
Epoch (UTC): | 11 August 2024 19:55:36 |
Eccentricity: | 0.0532885 |
inclination: | 63.3883° |
perigee height: | 707 km |
apogee height: | 1504 km |
right ascension of ascending node: | 118.0766° |
argument of perigee: | 3.9106° |
revolutions per day: | 13.41016672 |
mean anomaly at epoch: | 356.0894° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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