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 49192U 26145.45446672 +.00000000 +00000-0 -63325-3 0 00007
2 49192 87.8937 324.7654 0001551 78.5978 281.5326 13.13468798 03
| Epoch (UTC): | 25 May 2026 10:54:25 |
| Eccentricity: | 0.0001551 |
| inclination: | 87.8937° |
| perigee height: | 1209 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7654° |
| argument of perigee: | 78.5978° |
| revolutions per day: | 13.13468798 |
| mean anomaly at epoch: | 281.5326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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