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 37168U 10048A 23088.55811896 .00001524 00000-0 19687-3 0 9998
2 37168 97.9125 307.1364 0000895 113.7134 301.7329 14.82382622675984
Epoch (UTC): | 29 March 2023 13:23:41 |
Eccentricity: | 0.0000895 |
inclination: | 97.9125° |
perigee height: | 621 km |
apogee height: | 622 km |
right ascension of ascending node: | 307.1364° |
argument of perigee: | 113.7134° |
revolutions per day: | 14.82382622 |
mean anomaly at epoch: | 301.7329° |
orbit number at epoch: | 67598 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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