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 48968U 26145.51625392 +.00000000 +00000-0 +16063-3 0 00008
2 48968 87.9106 231.1094 0001930 129.7407 230.3899 13.25832337 02
| Epoch (UTC): | 25 May 2026 12:23:24 |
| Eccentricity: | 0.0001930 |
| inclination: | 87.9106° |
| perigee height: | 1161 km |
| apogee height: | 1164 km |
| right ascension of ascending node: | 231.1094° |
| argument of perigee: | 129.7407° |
| revolutions per day: | 13.25832337 |
| mean anomaly at epoch: | 230.3899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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