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 68235U 26145.50003470 +.00000000 +00000-0 +75079-5 0 00007
2 68235 53.1586 293.6818 0000576 87.0119 189.6015 15.34395750 07
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0000576 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 293.6818° |
| argument of perigee: | 87.0119° |
| revolutions per day: | 15.34395750 |
| mean anomaly at epoch: | 189.6015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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