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 68297U 26145.34878102 +.00000000 +00000-0 +10518-2 0 00003
2 68297 97.2850 271.6157 0001709 84.3777 275.7683 15.75250863 07
| Epoch (UTC): | 25 May 2026 08:22:14 |
| Eccentricity: | 0.0001709 |
| inclination: | 97.2850° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6157° |
| argument of perigee: | 84.3777° |
| revolutions per day: | 15.75250863 |
| mean anomaly at epoch: | 275.7683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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