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 68646U 26144.79814617 +.00000000 +00000-0 -29898+1 0 00000
2 68646 88.9877 323.4013 0004096 138.7087 221.4380 13.60932334 02
| Epoch (UTC): | 24 May 2026 19:09:19 |
| Eccentricity: | 0.0004096 |
| inclination: | 88.9877° |
| perigee height: | 1029 km |
| apogee height: | 1035 km |
| right ascension of ascending node: | 323.4013° |
| argument of perigee: | 138.7087° |
| revolutions per day: | 13.60932334 |
| mean anomaly at epoch: | 221.4380° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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