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 68586U 26145.11305259 +.00000000 +00000-0 +84254-3 0 00006
2 68586 51.8767 288.2860 0000996 253.9841 106.1036 15.37705540 03
| Epoch (UTC): | 25 May 2026 02:42:47 |
| Eccentricity: | 0.0000996 |
| inclination: | 51.8767° |
| perigee height: | 452 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 288.2860° |
| argument of perigee: | 253.9841° |
| revolutions per day: | 15.37705540 |
| mean anomaly at epoch: | 106.1036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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