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 55955U 26145.53974103 +.00000000 +00000-0 +60952-4 0 00008
2 55955 70.0006 70.7292 0003052 270.3892 89.6918 14.98340708 07
| Epoch (UTC): | 25 May 2026 12:57:13 |
| Eccentricity: | 0.0003052 |
| inclination: | 70.0006° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.7292° |
| argument of perigee: | 270.3892° |
| revolutions per day: | 14.98340708 |
| mean anomaly at epoch: | 89.6918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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