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 49203U 26145.41540281 +.00000000 +00000-0 +78267-3 0 00007
2 49203 87.8937 324.7717 0001819 97.8898 262.2437 13.13468479 03
| Epoch (UTC): | 25 May 2026 09:58:10 |
| Eccentricity: | 0.0001819 |
| inclination: | 87.8937° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7717° |
| argument of perigee: | 97.8898° |
| revolutions per day: | 13.13468479 |
| mean anomaly at epoch: | 262.2437° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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