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 68354U 26145.36569931 +.00000000 +00000-0 +64185-4 0 00007
2 68354 54.9757 128.9918 0013021 93.4459 266.8029 14.73290319 06
| Epoch (UTC): | 25 May 2026 08:46:36 |
| Eccentricity: | 0.0013021 |
| inclination: | 54.9757° |
| perigee height: | 641 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 128.9918° |
| argument of perigee: | 93.4459° |
| revolutions per day: | 14.73290319 |
| mean anomaly at epoch: | 266.8029° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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