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 05707U 71114B 24282.83866116 .00001678 00000-0 54053-3 0 9992
2 05707 74.0285 196.8464 0024744 330.2346 29.7399 14.39879955766735
Epoch (UTC): | 08 October 2024 20:07:40 |
Eccentricity: | 0.0024744 |
inclination: | 74.0285° |
perigee height: | 741 km |
apogee height: | 776 km |
right ascension of ascending node: | 196.8464° |
argument of perigee: | 330.2346° |
revolutions per day: | 14.39879955 |
mean anomaly at epoch: | 29.7399° |
orbit number at epoch: | 76673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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