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 68189U 26145.08579703 +.00000000 +00000-0 +82638-3 0 00002
2 68189 53.1590 271.6195 0001139 65.9952 294.1170 15.34377948 03
| Epoch (UTC): | 25 May 2026 02:03:32 |
| Eccentricity: | 0.0001139 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 271.6195° |
| argument of perigee: | 65.9952° |
| revolutions per day: | 15.34377948 |
| mean anomaly at epoch: | 294.1170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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