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 55632U 26145.36797059 +.00000000 +00000-0 -45990-4 0 00000
2 55632 69.9998 11.1324 0002699 268.2762 91.8088 14.98335188 08
| Epoch (UTC): | 25 May 2026 08:49:52 |
| Eccentricity: | 0.0002699 |
| inclination: | 69.9998° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 11.1324° |
| argument of perigee: | 268.2762° |
| revolutions per day: | 14.98335188 |
| mean anomaly at epoch: | 91.8088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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