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 41793U 26066.64029248 +.00000000 +00000-0 +00000-0 0 00002
2 41793 0.0190 149.9630 0003408 251.2377 68.6138 1.00271904 06
| Epoch (UTC): | 07 March 2026 15:22:01 |
| Eccentricity: | 0.0003408 |
| inclination: | 0.0190° |
| perigee height: | 35772 km |
| apogee height: | 35801 km |
| right ascension of ascending node: | 149.9630° |
| argument of perigee: | 251.2377° |
| revolutions per day: | 1.00271904 |
| mean anomaly at epoch: | 68.6138° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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