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 05435U 26106.94022958 +.00000000 +00000-0 +75952-4 0 00006
2 05435 50.1406 338.1987 0101876 313.5589 45.6915 14.60210586 04
| Epoch (UTC): | 16 April 2026 22:33:55 |
| Eccentricity: | 0.0101876 |
| inclination: | 50.1406° |
| perigee height: | 620 km |
| apogee height: | 765 km |
| right ascension of ascending node: | 338.1987° |
| argument of perigee: | 313.5589° |
| revolutions per day: | 14.60210586 |
| mean anomaly at epoch: | 45.6915° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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