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 41591U 26145.54280769 +.00000000 +00000-0 +00000-0 0 00002
2 41591 0.0181 295.2269 0002094 124.4594 169.3481 1.00271260 02
| Epoch (UTC): | 25 May 2026 13:01:38 |
| Eccentricity: | 0.0002094 |
| inclination: | 0.0181° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 295.2269° |
| argument of perigee: | 124.4594° |
| revolutions per day: | 1.00271260 |
| mean anomaly at epoch: | 169.3481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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