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 26076.26914698 +.00000000 +00000-0 +76854-5 0 00000
2 11608 81.2172 349.7156 0053573 184.1775 175.8954 14.06552784 01
| Epoch (UTC): | 17 March 2026 06:27:34 |
| Eccentricity: | 0.0053573 |
| inclination: | 81.2172° |
| perigee height: | 832 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 349.7156° |
| argument of perigee: | 184.1775° |
| revolutions per day: | 14.06552784 |
| mean anomaly at epoch: | 175.8954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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