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 49198U 26145.23231280 +.00000000 +00000-0 +72412-4 0 00003
2 49198 87.9170 340.0175 0002151 92.5418 267.5960 13.18686507 03
| Epoch (UTC): | 25 May 2026 05:34:31 |
| Eccentricity: | 0.0002151 |
| inclination: | 87.9170° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 340.0175° |
| argument of perigee: | 92.5418° |
| revolutions per day: | 13.18686507 |
| mean anomaly at epoch: | 267.5960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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