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 49169U 26145.27489439 +.00000000 +00000-0 +26590-4 0 00002
2 49169 70.0001 81.3682 0003057 270.5780 89.5029 14.98333673 01
| Epoch (UTC): | 25 May 2026 06:35:50 |
| Eccentricity: | 0.0003057 |
| inclination: | 70.0001° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.3682° |
| argument of perigee: | 270.5780° |
| revolutions per day: | 14.98333673 |
| mean anomaly at epoch: | 89.5029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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