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 21048U 91001B 24276.75308010 .00000626 00000-0 88480-3 0 9996
2 21048 18.4634 318.7301 1188298 273.6274 72.9241 11.85396186462841
Epoch (UTC): | 02 October 2024 18:04:26 |
Eccentricity: | 0.1188298 |
inclination: | 18.4634° |
perigee height: | 781 km |
apogee height: | 2712 km |
right ascension of ascending node: | 318.7301° |
argument of perigee: | 273.6274° |
revolutions per day: | 11.85396186 |
mean anomaly at epoch: | 72.9241° |
orbit number at epoch: | 46284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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