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 68651U 26144.79417895 +.00000000 +00000-0 +40587-4 0 00004
2 68651 88.9877 323.4002 0009437 68.2098 292.0064 13.63877759 04
| Epoch (UTC): | 24 May 2026 19:03:37 |
| Eccentricity: | 0.0009437 |
| inclination: | 88.9877° |
| perigee height: | 1015 km |
| apogee height: | 1029 km |
| right ascension of ascending node: | 323.4002° |
| argument of perigee: | 68.2098° |
| revolutions per day: | 13.63877759 |
| mean anomaly at epoch: | 292.0064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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