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 26159.30181865 +.00000000 +00000-0 +18028-3 0 00008
2 41634 75.0037 295.7939 0007060 51.7874 308.3949 14.93550036 03
| Epoch (UTC): | 08 June 2026 07:14:37 |
| Eccentricity: | 0.0007060 |
| inclination: | 75.0037° |
| perigee height: | 582 km |
| apogee height: | 592 km |
| right ascension of ascending node: | 295.7939° |
| argument of perigee: | 51.7874° |
| revolutions per day: | 14.93550036 |
| mean anomaly at epoch: | 308.3949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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