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 41105U 26032.41639124 +.00000000 +00000-0 +00000-0 0 00007
2 41105 6.3518 72.2062 0003779 222.8522 331.9465 1.00271780 01
| Epoch (UTC): | 01 February 2026 09:59:36 |
| Eccentricity: | 0.0003779 |
| inclination: | 6.3518° |
| perigee height: | 35771 km |
| apogee height: | 35803 km |
| right ascension of ascending node: | 72.2062° |
| argument of perigee: | 222.8522° |
| revolutions per day: | 1.00271780 |
| mean anomaly at epoch: | 331.9465° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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