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 55343U 26144.96869694 +.00000000 +00000-0 -12593-3 0 00001
2 55343 43.0049 232.2581 0002837 263.3779 96.6750 15.27594830 09
| Epoch (UTC): | 24 May 2026 23:14:55 |
| Eccentricity: | 0.0002837 |
| inclination: | 43.0049° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 232.2581° |
| argument of perigee: | 263.3779° |
| revolutions per day: | 15.27594830 |
| mean anomaly at epoch: | 96.6750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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