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 68185U 26145.35046204 +.00000000 +00000-0 +10251-2 0 00004
2 68185 53.1603 269.7171 0000578 38.5398 321.5646 15.34422680 09
| Epoch (UTC): | 25 May 2026 08:24:39 |
| Eccentricity: | 0.0000578 |
| inclination: | 53.1603° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 269.7171° |
| argument of perigee: | 38.5398° |
| revolutions per day: | 15.34422680 |
| mean anomaly at epoch: | 321.5646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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