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 40012U 14033C 24263.02017708 .00004946 00000-0 62729-3 0 9992
2 40012 97.7140 61.7492 0051357 359.9921 0.1282 14.81227195551728
Epoch (UTC): | 19 September 2024 00:29:03 |
Eccentricity: | 0.0051357 |
inclination: | 97.7140° |
perigee height: | 589 km |
apogee height: | 661 km |
right ascension of ascending node: | 61.7492° |
argument of perigee: | 359.9921° |
revolutions per day: | 14.81227195 |
mean anomaly at epoch: | 0.1282° |
orbit number at epoch: | 55172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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