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 41634U 26145.63668279 +.00000000 +00000-0 +76087-4 0 00008
2 41634 75.0032 321.6618 0006922 90.1015 270.0967 14.93508015 06
| Epoch (UTC): | 25 May 2026 15:16:49 |
| Eccentricity: | 0.0006922 |
| inclination: | 75.0032° |
| perigee height: | 582 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 321.6618° |
| argument of perigee: | 90.1015° |
| revolutions per day: | 14.93508015 |
| mean anomaly at epoch: | 270.0967° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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