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 26106.41712381 +.00000000 +00000-0 +11348-4 0 00008
2 05485 32.0575 10.4088 0639508 350.6037 8.3069 12.74248526 09
| Epoch (UTC): | 16 April 2026 10:00:39 |
| Eccentricity: | 0.0639508 |
| inclination: | 32.0575° |
| perigee height: | 870 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 10.4088° |
| argument of perigee: | 350.6037° |
| revolutions per day: | 12.74248526 |
| mean anomaly at epoch: | 8.3069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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