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 11672U 80005B 24280.84169736 .00003191 00000-0 32930-3 0 9994
2 11672 82.5125 78.9970 0017549 92.5210 267.8017 14.89787221399200
| Epoch (UTC): | 06 October 2024 20:12:02 |
| Eccentricity: | 0.0017549 |
| inclination: | 82.5125° |
| perigee height: | 586 km |
| apogee height: | 611 km |
| right ascension of ascending node: | 78.9970° |
| argument of perigee: | 92.5210° |
| revolutions per day: | 14.89787221 |
| mean anomaly at epoch: | 267.8017° |
| orbit number at epoch: | 39920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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