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 26140.28451594 +.00000000 +00000-0 +73011-3 0 00001
2 16591 63.2925 335.3391 0666905 112.6104 254.6887 14.14196836 08
| Epoch (UTC): | 20 May 2026 06:49:42 |
| Eccentricity: | 0.0666905 |
| inclination: | 63.2925° |
| perigee height: | 363 km |
| apogee height: | 1327 km |
| right ascension of ascending node: | 335.3391° |
| argument of perigee: | 112.6104° |
| revolutions per day: | 14.14196836 |
| mean anomaly at epoch: | 254.6887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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