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 26022.49632242 +.00000000 +00000-0 +20990-3 0 00008
2 41634 75.0019 194.6595 0006827 22.2243 337.9241 14.93034963 00
| Epoch (UTC): | 22 January 2026 11:54:42 |
| Eccentricity: | 0.0006827 |
| inclination: | 75.0019° |
| perigee height: | 584 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 194.6595° |
| argument of perigee: | 22.2243° |
| revolutions per day: | 14.93034963 |
| mean anomaly at epoch: | 337.9241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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