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 49166U 26145.52530213 +.00000000 +00000-0 +22920-4 0 00007
2 49166 70.0006 81.7621 0003122 269.7962 90.2839 14.97519424 02
| Epoch (UTC): | 25 May 2026 12:36:26 |
| Eccentricity: | 0.0003122 |
| inclination: | 70.0006° |
| perigee height: | 572 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 81.7621° |
| argument of perigee: | 269.7962° |
| revolutions per day: | 14.97519424 |
| mean anomaly at epoch: | 90.2839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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