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 49189U 26145.23017310 +.00000000 +00000-0 -46481-3 0 00006
2 49189 87.8940 324.8090 0001906 94.3288 265.8059 13.13469416 08
| Epoch (UTC): | 25 May 2026 05:31:26 |
| Eccentricity: | 0.0001906 |
| inclination: | 87.8940° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.8090° |
| argument of perigee: | 94.3288° |
| revolutions per day: | 13.13469416 |
| mean anomaly at epoch: | 265.8059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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