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 16613U 26160.28995102 +.00000000 +00000-0 +15843-3 0 00005
2 16613 98.6629 92.9655 0127333 290.3041 68.4517 14.71492247 05
| Epoch (UTC): | 09 June 2026 06:57:31 |
| Eccentricity: | 0.0127333 |
| inclination: | 98.6629° |
| perigee height: | 567 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 92.9655° |
| argument of perigee: | 290.3041° |
| revolutions per day: | 14.71492247 |
| mean anomaly at epoch: | 68.4517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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