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 68784U 26145.58335647 +.00000000 +00000-0 -28793-1 0 00006
2 68784 97.2847 182.4292 0001627 78.3274 37.0714 15.56606899 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001627 |
| inclination: | 97.2847° |
| perigee height: | 396 km |
| apogee height: | 399 km |
| right ascension of ascending node: | 182.4292° |
| argument of perigee: | 78.3274° |
| revolutions per day: | 15.56606899 |
| mean anomaly at epoch: | 37.0714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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