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 00053U 60009E 24313.78491869 -.00000059 00000-0 26068-3 0 9998
2 00053 47.2786 348.0690 0098506 146.7313 213.9717 12.17355095864115
Epoch (UTC): | 08 November 2024 18:50:16 |
Eccentricity: | 0.0098506 |
inclination: | 47.2786° |
perigee height: | 1525 km |
apogee height: | 1683 km |
right ascension of ascending node: | 348.0690° |
argument of perigee: | 146.7313° |
revolutions per day: | 12.17355095 |
mean anomaly at epoch: | 213.9717° |
orbit number at epoch: | 86411 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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