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 68356U 26145.63645139 +.00000000 +00000-0 +19555-4 0 00005
2 68356 54.9885 127.9593 0012338 78.4220 281.8163 14.73181034 06
| Epoch (UTC): | 25 May 2026 15:16:29 |
| Eccentricity: | 0.0012338 |
| inclination: | 54.9885° |
| perigee height: | 642 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 127.9593° |
| argument of perigee: | 78.4220° |
| revolutions per day: | 14.73181034 |
| mean anomaly at epoch: | 281.8163° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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