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 is defined by the following mean orbital elements,
1 11870U 26022.21708113 +.00000000 +00000-0 +20586-3 0 00009
2 11870 74.0513 195.6686 0014975 86.2019 274.0847 14.38354805 05
| Epoch (UTC): | 22 January 2026 05:12:35 |
| Eccentricity: | 0.0014975 |
| inclination: | 74.0513° |
| perigee height: | 753 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 195.6686° |
| argument of perigee: | 86.2019° |
| revolutions per day: | 14.38354805 |
| mean anomaly at epoch: | 274.0847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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