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 41310U 26075.78091154 +.00000000 +00000-0 +00000-0 0 00007
2 41310 0.0528 70.1837 0004121 262.8401 131.4555 1.00273330 06
| Epoch (UTC): | 16 March 2026 18:44:30 |
| Eccentricity: | 0.0004121 |
| inclination: | 0.0528° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 70.1837° |
| argument of perigee: | 262.8401° |
| revolutions per day: | 1.00273330 |
| mean anomaly at epoch: | 131.4555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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