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 65128U 26145.63815205 +.00000000 +00000-0 +18997-3 0 00000
2 65128 49.9779 231.6670 0025607 204.8937 155.0767 14.82002255 07
| Epoch (UTC): | 25 May 2026 15:18:56 |
| Eccentricity: | 0.0025607 |
| inclination: | 49.9779° |
| perigee height: | 605 km |
| apogee height: | 641 km |
| right ascension of ascending node: | 231.6670° |
| argument of perigee: | 204.8937° |
| revolutions per day: | 14.82002255 |
| mean anomaly at epoch: | 155.0767° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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