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 34941U 26145.60519946 +.00000000 +00000-0 +00000-0 0 00002
2 34941 0.0773 82.9882 0000694 314.8188 171.4988 1.00269837 03
| Epoch (UTC): | 25 May 2026 14:31:29 |
| Eccentricity: | 0.0000694 |
| inclination: | 0.0773° |
| perigee height: | 35784 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 82.9882° |
| argument of perigee: | 314.8188° |
| revolutions per day: | 1.00269837 |
| mean anomaly at epoch: | 171.4988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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