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 68282U 26145.21585779 +.00000000 +00000-0 +84355-3 0 00009
2 68282 53.1604 322.6388 0001172 85.1251 274.9885 15.34402010 05
| Epoch (UTC): | 25 May 2026 05:10:50 |
| Eccentricity: | 0.0001172 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 322.6388° |
| argument of perigee: | 85.1251° |
| revolutions per day: | 15.34402010 |
| mean anomaly at epoch: | 274.9885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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