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 68236U 26145.44273110 +.00000000 +00000-0 +86456-3 0 00000
2 68236 53.1591 298.2303 0001323 88.6323 271.4835 15.42190916 05
| Epoch (UTC): | 25 May 2026 10:37:31 |
| Eccentricity: | 0.0001323 |
| inclination: | 53.1591° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 298.2303° |
| argument of perigee: | 88.6323° |
| revolutions per day: | 15.42190916 |
| mean anomaly at epoch: | 271.4835° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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