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 68741U 26145.58335647 +.00000000 +00000-0 +15843-2 0 00001
2 68741 97.2851 9.2113 0001445 86.4456 190.6594 15.49143169 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001445 |
| inclination: | 97.2851° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 9.2113° |
| argument of perigee: | 86.4456° |
| revolutions per day: | 15.49143169 |
| mean anomaly at epoch: | 190.6594° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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