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 11870U 80056B 24287.50379842 .00000978 00000-0 33240-3 0 9996
2 11870 74.0538 332.7360 0016871 336.0958 23.9410 14.37870642295262
| Epoch (UTC): | 13 October 2024 12:05:28 |
| Eccentricity: | 0.0016871 |
| inclination: | 74.0538° |
| perigee height: | 753 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 332.7360° |
| argument of perigee: | 336.0958° |
| revolutions per day: | 14.37870642 |
| mean anomaly at epoch: | 23.9410° |
| orbit number at epoch: | 29526 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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