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 55943U 26145.26874270 +.00000000 +00000-0 +26501-4 0 00001
2 55943 69.9998 91.2592 0003096 269.4395 90.6409 14.98332566 07
| Epoch (UTC): | 25 May 2026 06:26:59 |
| Eccentricity: | 0.0003096 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 91.2592° |
| argument of perigee: | 269.4395° |
| revolutions per day: | 14.98332566 |
| mean anomaly at epoch: | 90.6409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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