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 37792U 11044E 23266.65834961 .00001820 00000-0 26092-3 0 9992
2 37792 98.2618 159.3044 0055952 327.2083 32.5658 14.76803666651470
| Epoch (UTC): | 23 September 2023 15:48:01 |
| Eccentricity: | 0.0055952 |
| inclination: | 98.2618° |
| perigee height: | 600 km |
| apogee height: | 679 km |
| right ascension of ascending node: | 159.3044° |
| argument of perigee: | 327.2083° |
| revolutions per day: | 14.76803666 |
| mean anomaly at epoch: | 32.5658° |
| orbit number at epoch: | 65147 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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