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 26150.43017088 +.00000000 +00000-0 +30568-3 0 00000
2 16613 98.6630 82.4731 0127798 321.4663 37.7469 14.71461338 09
| Epoch (UTC): | 30 May 2026 10:19:26 |
| Eccentricity: | 0.0127798 |
| inclination: | 98.6630° |
| perigee height: | 567 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 82.4731° |
| argument of perigee: | 321.4663° |
| revolutions per day: | 14.71461338 |
| mean anomaly at epoch: | 37.7469° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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