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 55990U 26145.59781102 +.00000000 +00000-0 +10877-4 0 00009
2 55990 43.0044 345.0973 0001096 272.6890 87.3836 15.27578819 04
| Epoch (UTC): | 25 May 2026 14:20:50 |
| Eccentricity: | 0.0001096 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.0973° |
| argument of perigee: | 272.6890° |
| revolutions per day: | 15.27578819 |
| mean anomaly at epoch: | 87.3836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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