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 56050U 26145.32505948 +.00000000 +00000-0 +22771-3 0 00005
2 56050 87.9104 233.3096 0002361 92.3516 267.7886 13.16594588 05
| Epoch (UTC): | 25 May 2026 07:48:05 |
| Eccentricity: | 0.0002361 |
| inclination: | 87.9104° |
| perigee height: | 1196 km |
| apogee height: | 1200 km |
| right ascension of ascending node: | 233.3096° |
| argument of perigee: | 92.3516° |
| revolutions per day: | 13.16594588 |
| mean anomaly at epoch: | 267.7886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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