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 00965U 26110.49585270 +.00000000 +00000-0 +67054-4 0 00009
2 00965 90.0798 202.5682 0043615 87.0738 284.2191 13.57007156 04
| Epoch (UTC): | 20 April 2026 11:54:01 |
| Eccentricity: | 0.0043615 |
| inclination: | 90.0798° |
| perigee height: | 1014 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 202.5682° |
| argument of perigee: | 87.0738° |
| revolutions per day: | 13.57007156 |
| mean anomaly at epoch: | 284.2191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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