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 68911U 26145.47683628 +.00000000 +00000-0 +98872-3 0 00007
2 68911 97.2868 341.2845 0002172 78.9845 281.1651 15.49229984 04
| Epoch (UTC): | 25 May 2026 11:26:38 |
| Eccentricity: | 0.0002172 |
| inclination: | 97.2868° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 341.2845° |
| argument of perigee: | 78.9845° |
| revolutions per day: | 15.49229984 |
| mean anomaly at epoch: | 281.1651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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