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 05485U 26104.14416531 +.00000000 +00000-0 +95133-6 0 00000
2 05485 32.0581 20.2432 0639614 335.5729 21.5770 12.74248515 00
| Epoch (UTC): | 14 April 2026 03:27:35 |
| Eccentricity: | 0.0639614 |
| inclination: | 32.0581° |
| perigee height: | 869 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 20.2432° |
| argument of perigee: | 335.5729° |
| revolutions per day: | 12.74248515 |
| mean anomaly at epoch: | 21.5770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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