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 68485U 26145.63285735 +.00000000 +00000-0 +70231-3 0 00007
2 68485 97.7561 104.2542 0002883 57.8330 302.3169 14.92253816 08
| Epoch (UTC): | 25 May 2026 15:11:18 |
| Eccentricity: | 0.0002883 |
| inclination: | 97.7561° |
| perigee height: | 589 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 104.2542° |
| argument of perigee: | 57.8330° |
| revolutions per day: | 14.92253816 |
| mean anomaly at epoch: | 302.3169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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