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 41586U 26145.60563279 +.00000000 +00000-0 +00000-0 0 00003
2 41586 1.6666 69.1329 0006912 355.7650 146.8017 1.00276127 03
| Epoch (UTC): | 25 May 2026 14:32:06 |
| Eccentricity: | 0.0006912 |
| inclination: | 1.6666° |
| perigee height: | 35756 km |
| apogee height: | 35815 km |
| right ascension of ascending node: | 69.1329° |
| argument of perigee: | 355.7650° |
| revolutions per day: | 1.00276127 |
| mean anomaly at epoch: | 146.8017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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