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 68645U 26144.78331284 +.00000000 +00000-0 -29371+1 0 00008
2 68645 88.9870 323.4163 0007496 71.6653 288.5316 13.57980142 00
| Epoch (UTC): | 24 May 2026 18:47:58 |
| Eccentricity: | 0.0007496 |
| inclination: | 88.9870° |
| perigee height: | 1037 km |
| apogee height: | 1049 km |
| right ascension of ascending node: | 323.4163° |
| argument of perigee: | 71.6653° |
| revolutions per day: | 13.57980142 |
| mean anomaly at epoch: | 288.5316° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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