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 46995U 99025EZV 23272.33903475 .00005370 00000-0 46462-2 0 9997
2 46995 98.5957 53.7892 0207754 144.7068 216.8044 13.77285356493443
Epoch (UTC): | 29 September 2023 08:08:12 |
Eccentricity: | 0.0207754 |
inclination: | 98.5957° |
perigee height: | 821 km |
apogee height: | 1126 km |
right ascension of ascending node: | 53.7892° |
argument of perigee: | 144.7068° |
revolutions per day: | 13.77285356 |
mean anomaly at epoch: | 216.8044° |
orbit number at epoch: | 49344 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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