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 28117U 03057A 23088.44516868 -.00000107 00000-0 00000+0 0 9995
2 28117 7.3903 37.6584 0004405 2.2644 22.4069 1.00273381 70631
Epoch (UTC): | 29 March 2023 10:41:02 |
Eccentricity: | 0.0004405 |
inclination: | 7.3903° |
perigee height: | 35767 km |
apogee height: | 35804 km |
right ascension of ascending node: | 37.6584° |
argument of perigee: | 2.2644° |
revolutions per day: | 1.00273381 |
mean anomaly at epoch: | 22.4069° |
orbit number at epoch: | 7063 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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