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 68867U 26145.52254713 +.00000000 +00000-0 -25835-2 0 00001
2 68867 51.8815 351.8895 0006543 195.9214 164.1568 15.37602110 00
| Epoch (UTC): | 25 May 2026 12:32:28 |
| Eccentricity: | 0.0006543 |
| inclination: | 51.8815° |
| perigee height: | 449 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 351.8895° |
| argument of perigee: | 195.9214° |
| revolutions per day: | 15.37602110 |
| mean anomaly at epoch: | 164.1568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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