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 23342.03382678 -.00000077 00000-0 00000+0 0 9999
2 28117 7.7690 37.2253 0002683 203.7438 282.8836 1.00272690 73170
Epoch (UTC): | 08 December 2023 00:48:42 |
Eccentricity: | 0.0002683 |
inclination: | 7.7690° |
perigee height: | 35774 km |
apogee height: | 35797 km |
right ascension of ascending node: | 37.2253° |
argument of perigee: | 203.7438° |
revolutions per day: | 1.00272690 |
mean anomaly at epoch: | 282.8836° |
orbit number at epoch: | 7317 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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