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 43651U 18079A 24284.46150701 -.00000270 00000-0 00000-0 0 9998
2 43651 1.6342 334.5836 0052314 8.9785 134.5717 1.00267996 22137
Epoch (UTC): | 10 October 2024 11:04:34 |
Eccentricity: | 0.0052314 |
inclination: | 1.6342° |
perigee height: | 35566 km |
apogee height: | 36008 km |
right ascension of ascending node: | 334.5836° |
argument of perigee: | 8.9785° |
revolutions per day: | 1.00267996 |
mean anomaly at epoch: | 134.5717° |
orbit number at epoch: | 2213 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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