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 26145.56318832 +.00000000 +00000-0 +00000-0 0 00002
2 41622 2.2509 301.2609 0195965 261.1088 138.3738 1.00268395 04
| Epoch (UTC): | 25 May 2026 13:30:59 |
| Eccentricity: | 0.0195965 |
| inclination: | 2.2509° |
| perigee height: | 34961 km |
| apogee height: | 36614 km |
| right ascension of ascending node: | 301.2609° |
| argument of perigee: | 261.1088° |
| revolutions per day: | 1.00268395 |
| mean anomaly at epoch: | 138.3738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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