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 26158.99908319 +.00000000 +00000-0 +42862-4 0 00005
2 11608 81.2140 269.3593 0052930 313.1509 46.5240 14.06566732 03
| Epoch (UTC): | 07 June 2026 23:58:40 |
| Eccentricity: | 0.0052930 |
| inclination: | 81.2140° |
| perigee height: | 833 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 269.3593° |
| argument of perigee: | 313.1509° |
| revolutions per day: | 14.06566732 |
| mean anomaly at epoch: | 46.5240° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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