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 23336.92591799 .00002215 00000-0 21231-3 0 9999
2 43678 98.0456 124.6448 0008767 330.9240 29.1490 14.94207252277456
| Epoch (UTC): | 02 December 2023 22:13:19 |
| Eccentricity: | 0.0008767 |
| inclination: | 98.0456° |
| perigee height: | 579 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 124.6448° |
| argument of perigee: | 330.9240° |
| revolutions per day: | 14.94207252 |
| mean anomaly at epoch: | 29.1490° |
| orbit number at epoch: | 27745 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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