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 37855U 11061F 23089.70431949 .00040125 00000-0 13876-2 0 9995
2 37855 101.7034 7.7145 0127609 279.9173 78.7664 15.22301644625079
| Epoch (UTC): | 30 March 2023 16:54:13 |
| Eccentricity: | 0.0127609 |
| inclination: | 101.7034° |
| perigee height: | 411 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 7.7145° |
| argument of perigee: | 279.9173° |
| revolutions per day: | 15.22301644 |
| mean anomaly at epoch: | 78.7664° |
| orbit number at epoch: | 62507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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