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 11608U 26020.14318770 +.00000000 +00000-0 +14843-4 0 00004
2 11608 81.2108 44.2245 0054013 344.3154 15.6339 14.06539464 05
| Epoch (UTC): | 20 January 2026 03:26:11 |
| Eccentricity: | 0.0054013 |
| inclination: | 81.2108° |
| perigee height: | 832 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 44.2245° |
| argument of perigee: | 344.3154° |
| revolutions per day: | 14.06539464 |
| mean anomaly at epoch: | 15.6339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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