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 68488U 26145.58335647 +.00000000 +00000-0 -38736-2 0 00006
2 68488 97.7561 104.1780 0003117 94.3287 306.5037 14.92923943 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003117 |
| inclination: | 97.7561° |
| perigee height: | 587 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 104.1780° |
| argument of perigee: | 94.3287° |
| revolutions per day: | 14.92923943 |
| mean anomaly at epoch: | 306.5037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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