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 57440C 23105L 24358.47826389 -.00013606 00000+0 -10041-2 0 3584
2 57440 43.0014 139.2022 0001420 267.3130 299.5753 15.02543367 19
| Epoch (UTC): | 23 December 2024 11:28:42 |
| Eccentricity: | 0.0001420 |
| inclination: | 43.0014° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 139.2022° |
| argument of perigee: | 267.3130° |
| revolutions per day: | 15.02543367 |
| mean anomaly at epoch: | 299.5753° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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