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 34275U 93036LV 23335.64288821 .00024944 00000-0 47608-2 0 9997
2 34275 74.0328 44.7550 0010627 301.4514 178.9461 14.63835627778683
Epoch (UTC): | 01 December 2023 15:25:45 |
Eccentricity: | 0.0010627 |
inclination: | 74.0328° |
perigee height: | 673 km |
apogee height: | 688 km |
right ascension of ascending node: | 44.7550° |
argument of perigee: | 301.4514° |
revolutions per day: | 14.63835627 |
mean anomaly at epoch: | 178.9461° |
orbit number at epoch: | 77868 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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