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 55686U 26144.75293683 +.00000000 +00000-0 +00000-0 0 00003
2 55686 0.0725 75.2166 0004177 1.4002 201.9001 1.00270844 08
| Epoch (UTC): | 24 May 2026 18:04:13 |
| Eccentricity: | 0.0004177 |
| inclination: | 0.0725° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 75.2166° |
| argument of perigee: | 1.4002° |
| revolutions per day: | 1.00270844 |
| mean anomaly at epoch: | 201.9001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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