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 41339U 26053.86265992 +.00000000 +00000-0 +28824-3 0 00003
2 41339 31.0067 357.9052 0009530 338.3594 21.6643 15.17423010 08
| Epoch (UTC): | 22 February 2026 20:42:13 |
| Eccentricity: | 0.0009530 |
| inclination: | 31.0067° |
| perigee height: | 507 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 357.9052° |
| argument of perigee: | 338.3594° |
| revolutions per day: | 15.17423010 |
| mean anomaly at epoch: | 21.6643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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