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 65950U 26145.65369528 +.00000000 +00000-0 +10836-3 0 00001
2 65950 51.8995 12.7521 0001116 104.1873 255.9213 14.79934367 05
| Epoch (UTC): | 25 May 2026 15:41:19 |
| Eccentricity: | 0.0001116 |
| inclination: | 51.8995° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 12.7521° |
| argument of perigee: | 104.1873° |
| revolutions per day: | 14.79934367 |
| mean anomaly at epoch: | 255.9213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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