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 40014U 14033E 24315.90036620 .00016076 00000-0 10556-2 0 9990
2 40014 98.1072 5.0882 0033444 2.7960 357.3447 15.07259689567714
Epoch (UTC): | 10 November 2024 21:36:31 |
Eccentricity: | 0.0033444 |
inclination: | 98.1072° |
perigee height: | 521 km |
apogee height: | 568 km |
right ascension of ascending node: | 5.0882° |
argument of perigee: | 2.7960° |
revolutions per day: | 15.07259689 |
mean anomaly at epoch: | 357.3447° |
orbit number at epoch: | 56771 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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