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 41430U 00055LK 24353.20772396 .00013924 00000-0 43398-2 0 9993
2 41430 99.0136 165.4601 0039073 327.5879 32.2908 14.40541725463211
Epoch (UTC): | 18 December 2024 04:59:07 |
Eccentricity: | 0.0039073 |
inclination: | 99.0136° |
perigee height: | 729 km |
apogee height: | 784 km |
right ascension of ascending node: | 165.4601° |
argument of perigee: | 327.5879° |
revolutions per day: | 14.40541725 |
mean anomaly at epoch: | 32.2908° |
orbit number at epoch: | 46321 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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