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 24357.88759269 .00004217 00000-0 37239-3 0 9995
2 43678 98.0883 161.8795 0010113 120.8856 239.3361 14.96909975335130
| Epoch (UTC): | 22 December 2024 21:18:08 |
| Eccentricity: | 0.0010113 |
| inclination: | 98.0883° |
| perigee height: | 569 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 161.8795° |
| argument of perigee: | 120.8856° |
| revolutions per day: | 14.96909975 |
| mean anomaly at epoch: | 239.3361° |
| orbit number at epoch: | 33513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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