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 26140.89676657 +.00000000 +00000-0 +83165-4 0 00009
2 05485 32.0555 221.2153 0639741 218.6674 136.6401 12.74250407 07
| Epoch (UTC): | 20 May 2026 21:31:20 |
| Eccentricity: | 0.0639741 |
| inclination: | 32.0555° |
| perigee height: | 869 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 221.2153° |
| argument of perigee: | 218.6674° |
| revolutions per day: | 12.74250407 |
| mean anomaly at epoch: | 136.6401° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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