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 68358U 26145.37770242 +.00000000 +00000-0 +26209-4 0 00006
2 68358 54.9791 129.0877 0011217 89.1373 271.0910 14.72831996 04
| Epoch (UTC): | 25 May 2026 09:03:53 |
| Eccentricity: | 0.0011217 |
| inclination: | 54.9791° |
| perigee height: | 644 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 129.0877° |
| argument of perigee: | 89.1373° |
| revolutions per day: | 14.72831996 |
| mean anomaly at epoch: | 271.0910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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