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 23342.14924759 .00001500 00000-0 14554-3 0 9992
2 43678 98.0456 129.9957 0008393 311.6948 48.3552 14.94225120278238
| Epoch (UTC): | 08 December 2023 03:34:54 |
| Eccentricity: | 0.0008393 |
| inclination: | 98.0456° |
| perigee height: | 579 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 129.9957° |
| argument of perigee: | 311.6948° |
| revolutions per day: | 14.94225120 |
| mean anomaly at epoch: | 48.3552° |
| orbit number at epoch: | 27823 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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