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 68656U 26144.58409529 +.00000000 +00000-0 -83699-3 0 00002
2 68656 86.4979 51.8734 0002625 81.2440 278.8997 13.34575222 02
| Epoch (UTC): | 24 May 2026 14:01:05 |
| Eccentricity: | 0.0002625 |
| inclination: | 86.4979° |
| perigee height: | 1128 km |
| apogee height: | 1132 km |
| right ascension of ascending node: | 51.8734° |
| argument of perigee: | 81.2440° |
| revolutions per day: | 13.34575222 |
| mean anomaly at epoch: | 278.8997° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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