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 31122U 26053.54648227 +.00000000 +00000-0 +41154-3 0 00004
2 31122 98.4129 52.1161 0063219 269.1626 90.2337 14.72505133 08
| Epoch (UTC): | 22 February 2026 13:06:56 |
| Eccentricity: | 0.0063219 |
| inclination: | 98.4129° |
| perigee height: | 609 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 52.1161° |
| argument of perigee: | 269.1626° |
| revolutions per day: | 14.72505133 |
| mean anomaly at epoch: | 90.2337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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