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 35755U 26145.60987948 +.00000000 +00000-0 +00000-0 0 00007
2 35755 0.0387 88.4533 0000519 255.9451 250.3798 1.00273091 09
| Epoch (UTC): | 25 May 2026 14:38:13 |
| Eccentricity: | 0.0000519 |
| inclination: | 0.0387° |
| perigee height: | 35784 km |
| apogee height: | 35788 km |
| right ascension of ascending node: | 88.4533° |
| argument of perigee: | 255.9451° |
| revolutions per day: | 1.00273091 |
| mean anomaly at epoch: | 250.3798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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