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 8709U 76019A 23082.70601010 .00000039 00000-0 10085-3 0 9996
2 8709 69.6723 78.1905 0013904 262.1601 269.5299 13.71512922355349
Epoch (UTC): | 23 March 2023 16:56:39 |
Eccentricity: | 0.0013904 |
inclination: | 69.6723° |
perigee height: | 984 km |
apogee height: | 1004 km |
right ascension of ascending node: | 78.1905° |
argument of perigee: | 262.1601° |
revolutions per day: | 13.71512922 |
mean anomaly at epoch: | 269.5299° |
orbit number at epoch: | 35534 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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