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 43678U 18084H 23342.55103991 .00001521 00000-0 14754-3 0 9999
2 43678 98.0456 130.4073 0008364 310.2104 49.8382 14.94226586278291
| Epoch (UTC): | 08 December 2023 13:13:29 |
| Eccentricity: | 0.0008364 |
| inclination: | 98.0456° |
| perigee height: | 579 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 130.4073° |
| argument of perigee: | 310.2104° |
| revolutions per day: | 14.94226586 |
| mean anomaly at epoch: | 49.8382° |
| orbit number at epoch: | 27829 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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