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 13205U 82045A 25304.74244421 .00000044 00000-0 00000-0 0 9990
2 13205 71.9842 75.1735 4968098 329.5011 9.1373 2.00464983318233
| Epoch (UTC): | 31 October 2025 17:49:07 |
| Eccentricity: | 0.4968098 |
| inclination: | 71.9842° |
| perigee height: | 6991 km |
| apogee height: | 33390 km |
| right ascension of ascending node: | 75.1735° |
| argument of perigee: | 329.5011° |
| revolutions per day: | 2.00464983 |
| mean anomaly at epoch: | 9.1373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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