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 41622U 26140.57252190 +.00000000 +00000-0 +00000-0 0 00002
2 41622 2.2624 301.1683 0195796 261.2545 136.8236 1.00267786 03
| Epoch (UTC): | 20 May 2026 13:44:25 |
| Eccentricity: | 0.0195796 |
| inclination: | 2.2624° |
| perigee height: | 34962 km |
| apogee height: | 36613 km |
| right ascension of ascending node: | 301.1683° |
| argument of perigee: | 261.2545° |
| revolutions per day: | 1.00267786 |
| mean anomaly at epoch: | 136.8236° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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