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 68353U 26145.44382985 +.00000000 +00000-0 +25632-4 0 00001
2 68353 54.9818 128.8174 0010260 91.8869 268.3305 14.73265720 07
| Epoch (UTC): | 25 May 2026 10:39:06 |
| Eccentricity: | 0.0010260 |
| inclination: | 54.9818° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 128.8174° |
| argument of perigee: | 91.8869° |
| revolutions per day: | 14.73265720 |
| mean anomaly at epoch: | 268.3305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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