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 36830U 26145.36845052 +.00000000 +00000-0 +00000-0 0 00004
2 36830 0.0327 124.7594 0003845 325.2360 278.6108 1.00270961 05
| Epoch (UTC): | 25 May 2026 08:50:34 |
| Eccentricity: | 0.0003845 |
| inclination: | 0.0327° |
| perigee height: | 35771 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 124.7594° |
| argument of perigee: | 325.2360° |
| revolutions per day: | 1.00270961 |
| mean anomaly at epoch: | 278.6108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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