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 47303U 20103B 24282.57019380 .00012808 00000-0 25302-2 0 9997
2 47303 98.1172 171.8734 0002730 15.5216 344.6069 14.62524115201501
Epoch (UTC): | 08 October 2024 13:41:04 |
Eccentricity: | 0.0002730 |
inclination: | 98.1172° |
perigee height: | 683 km |
apogee height: | 687 km |
right ascension of ascending node: | 171.8734° |
argument of perigee: | 15.5216° |
revolutions per day: | 14.62524115 |
mean anomaly at epoch: | 344.6069° |
orbit number at epoch: | 20150 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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