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 10761U 26040.96618308 +.00000000 +00000-0 +42960-1 0 00003
2 10761 101.3493 303.0118 0040013 162.0705 198.1972 15.83644780 06
| Epoch (UTC): | 09 February 2026 23:11:18 |
| Eccentricity: | 0.0040013 |
| inclination: | 101.3493° |
| perigee height: | 293 km |
| apogee height: | 347 km |
| right ascension of ascending node: | 303.0118° |
| argument of perigee: | 162.0705° |
| revolutions per day: | 15.83644780 |
| mean anomaly at epoch: | 198.1972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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