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 26072.92576867 +.00000000 +00000-0 +18766-4 0 00008
2 11608 81.2173 352.9612 0053391 193.4296 166.5456 14.06552630 08
| Epoch (UTC): | 13 March 2026 22:13:06 |
| Eccentricity: | 0.0053391 |
| inclination: | 81.2173° |
| perigee height: | 832 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 352.9612° |
| argument of perigee: | 193.4296° |
| revolutions per day: | 14.06552630 |
| mean anomaly at epoch: | 166.5456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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