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 43679U 18084J 23342.89780959 .00003900 00000-0 32658-3 0 9998
2 43679 98.0413 135.1432 0006599 297.2559 62.7990 14.99044860278581
| Epoch (UTC): | 08 December 2023 21:32:50 |
| Eccentricity: | 0.0006599 |
| inclination: | 98.0413° |
| perigee height: | 565 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 135.1432° |
| argument of perigee: | 297.2559° |
| revolutions per day: | 14.99044860 |
| mean anomaly at epoch: | 62.7990° |
| orbit number at epoch: | 27858 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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