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 17973U 87041A 24276.79094717 .00000685 00000-0 38134-3 0 9993
2 17973 70.8987 56.9654 0028914 87.4855 272.9576 14.14373247929648
Epoch (UTC): | 02 October 2024 18:58:57 |
Eccentricity: | 0.0028914 |
inclination: | 70.8987° |
perigee height: | 823 km |
apogee height: | 865 km |
right ascension of ascending node: | 56.9654° |
argument of perigee: | 87.4855° |
revolutions per day: | 14.14373247 |
mean anomaly at epoch: | 272.9576° |
orbit number at epoch: | 92964 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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