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 55936U 26145.50634686 +.00000000 +00000-0 -25687-5 0 00001
2 55936 70.0010 70.6123 0002833 274.2768 85.8067 14.98328903 00
| Epoch (UTC): | 25 May 2026 12:09:08 |
| Eccentricity: | 0.0002833 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 70.6123° |
| argument of perigee: | 274.2768° |
| revolutions per day: | 14.98328903 |
| mean anomaly at epoch: | 85.8067° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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