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 45985U 26145.38899062 +.00000000 +00000-0 +00000-0 0 00007
2 45985 0.0126 291.3681 0000833 22.3805 165.7664 1.00272734 07
| Epoch (UTC): | 25 May 2026 09:20:08 |
| Eccentricity: | 0.0000833 |
| inclination: | 0.0126° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 291.3681° |
| argument of perigee: | 22.3805° |
| revolutions per day: | 1.00272734 |
| mean anomaly at epoch: | 165.7664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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