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 26150.83384241 +.00000000 +00000-0 +22811-3 0 00000
2 31126 98.4289 118.3793 0083048 102.1898 258.8620 14.62624797 08
| Epoch (UTC): | 30 May 2026 20:00:43 |
| Eccentricity: | 0.0083048 |
| inclination: | 98.4289° |
| perigee height: | 626 km |
| apogee height: | 743 km |
| right ascension of ascending node: | 118.3793° |
| argument of perigee: | 102.1898° |
| revolutions per day: | 14.62624797 |
| mean anomaly at epoch: | 258.8620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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