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 43880U 18111E 24261.18733575 .00058449 00000-0 32941-2 0 9990
2 43880 97.6007 166.3694 0018069 59.3589 300.9420 15.12826186311320
| Epoch (UTC): | 17 September 2024 04:29:45 |
| Eccentricity: | 0.0018069 |
| inclination: | 97.6007° |
| perigee height: | 515 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 166.3694° |
| argument of perigee: | 59.3589° |
| revolutions per day: | 15.12826186 |
| mean anomaly at epoch: | 300.9420° |
| orbit number at epoch: | 31132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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