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 43677U 18084G 23334.09564831 .00005564 00000-0 52350-3 0 9997
2 43677 98.0365 117.4089 0013948 324.8469 35.1829 14.94231363276820
| Epoch (UTC): | 30 November 2023 02:17:44 |
| Eccentricity: | 0.0013948 |
| inclination: | 98.0365° |
| perigee height: | 575 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 117.4089° |
| argument of perigee: | 324.8469° |
| revolutions per day: | 14.94231363 |
| mean anomaly at epoch: | 35.1829° |
| orbit number at epoch: | 27682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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