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 26088.14880602 +.00000000 +00000-0 +90303-4 0 00001
2 11608 81.2155 338.1818 0054102 151.3569 209.0591 14.06554307 05
| Epoch (UTC): | 29 March 2026 03:34:16 |
| Eccentricity: | 0.0054102 |
| inclination: | 81.2155° |
| perigee height: | 832 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 338.1818° |
| argument of perigee: | 151.3569° |
| revolutions per day: | 14.06554307 |
| mean anomaly at epoch: | 209.0591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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