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 41034U 26145.60918612 +.00000000 +00000-0 +00000-0 0 00006
2 41034 0.0052 105.0609 0002567 282.3786 203.5729 1.00271693 05
| Epoch (UTC): | 25 May 2026 14:37:13 |
| Eccentricity: | 0.0002567 |
| inclination: | 0.0052° |
| perigee height: | 35776 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 105.0609° |
| argument of perigee: | 282.3786° |
| revolutions per day: | 1.00271693 |
| mean anomaly at epoch: | 203.5729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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