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 39122U 26145.56058831 +.00000000 +00000-0 +00000-0 0 00004
2 39122 0.0158 352.7699 0002680 69.0973 266.2801 1.00272035 09
| Epoch (UTC): | 25 May 2026 13:27:14 |
| Eccentricity: | 0.0002680 |
| inclination: | 0.0158° |
| perigee height: | 35775 km |
| apogee height: | 35798 km |
| right ascension of ascending node: | 352.7699° |
| argument of perigee: | 69.0973° |
| revolutions per day: | 1.00272035 |
| mean anomaly at epoch: | 266.2801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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