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 23089.52180839 .00002784 00000-0 27261-3 0 9999
2 43678 98.0077 231.9804 0010814 63.7378 296.4888 14.93100294240527
| Epoch (UTC): | 30 March 2023 12:31:24 |
| Eccentricity: | 0.0010814 |
| inclination: | 98.0077° |
| perigee height: | 581 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 231.9804° |
| argument of perigee: | 63.7378° |
| revolutions per day: | 14.93100294 |
| mean anomaly at epoch: | 296.4888° |
| orbit number at epoch: | 24052 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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