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 16591U 26146.22382608 +.00000000 +00000-0 +10802-2 0 00008
2 16591 63.2939 317.9806 0665629 112.7262 254.5535 14.14410277 05
| Epoch (UTC): | 26 May 2026 05:22:18 |
| Eccentricity: | 0.0665629 |
| inclination: | 63.2939° |
| perigee height: | 364 km |
| apogee height: | 1325 km |
| right ascension of ascending node: | 317.9806° |
| argument of perigee: | 112.7262° |
| revolutions per day: | 14.14410277 |
| mean anomaly at epoch: | 254.5535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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