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 68998U 26145.26406869 +.00000000 +00000-0 +13350-3 0 00007
2 68998 97.7418 43.1589 0002743 127.4169 232.7300 14.91919370 05
| Epoch (UTC): | 25 May 2026 06:20:15 |
| Eccentricity: | 0.0002743 |
| inclination: | 97.7418° |
| perigee height: | 590 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 43.1589° |
| argument of perigee: | 127.4169° |
| revolutions per day: | 14.91919370 |
| mean anomaly at epoch: | 232.7300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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