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 55271U 26145.59977399 +.00000000 +00000-0 +10722-4 0 00005
2 55271 69.9990 210.6427 0003656 269.8387 90.2353 14.98333680 06
| Epoch (UTC): | 25 May 2026 14:23:40 |
| Eccentricity: | 0.0003656 |
| inclination: | 69.9990° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 210.6427° |
| argument of perigee: | 269.8387° |
| revolutions per day: | 14.98333680 |
| mean anomaly at epoch: | 90.2353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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