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 12786U 81082B 24284.55567313 .00001885 00000-0 21117-3 0 9995
2 12786 82.4883 327.7862 0018472 71.4497 288.8724 14.86254636310321
| Epoch (UTC): | 10 October 2024 13:20:10 |
| Eccentricity: | 0.0018472 |
| inclination: | 82.4883° |
| perigee height: | 597 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 327.7862° |
| argument of perigee: | 71.4497° |
| revolutions per day: | 14.86254636 |
| mean anomaly at epoch: | 288.8724° |
| orbit number at epoch: | 31032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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