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 49186U 26145.38844522 +.00000000 +00000-0 -62387-5 0 00007
2 49186 87.8930 324.7825 0001993 91.9345 268.2012 13.13469196 03
| Epoch (UTC): | 25 May 2026 09:19:21 |
| Eccentricity: | 0.0001993 |
| inclination: | 87.8930° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7825° |
| argument of perigee: | 91.9345° |
| revolutions per day: | 13.13469196 |
| mean anomaly at epoch: | 268.2012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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