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 55668U 26144.93356625 +.00000000 +00000-0 +20869-4 0 00008
2 55668 69.9996 332.2772 0002860 265.4819 94.6013 14.98330567 06
| Epoch (UTC): | 24 May 2026 22:24:20 |
| Eccentricity: | 0.0002860 |
| inclination: | 69.9996° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 332.2772° |
| argument of perigee: | 265.4819° |
| revolutions per day: | 14.98330567 |
| mean anomaly at epoch: | 94.6013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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