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 31126U 26103.62901883 +.00000000 +00000-0 +10035-3 0 00007
2 31126 98.4247 70.1984 0080572 249.0583 110.1981 14.62560740 07
| Epoch (UTC): | 13 April 2026 15:05:47 |
| Eccentricity: | 0.0080572 |
| inclination: | 98.4247° |
| perigee height: | 628 km |
| apogee height: | 742 km |
| right ascension of ascending node: | 70.1984° |
| argument of perigee: | 249.0583° |
| revolutions per day: | 14.62560740 |
| mean anomaly at epoch: | 110.1981° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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