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 26160.27950069 +.00000000 +00000-0 +11458-4 0 00005
2 11608 81.2140 268.1159 0052822 309.5332 50.1174 14.06566784 05
| Epoch (UTC): | 09 June 2026 06:42:28 |
| Eccentricity: | 0.0052822 |
| inclination: | 81.2140° |
| perigee height: | 833 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 268.1159° |
| argument of perigee: | 309.5332° |
| revolutions per day: | 14.06566784 |
| mean anomaly at epoch: | 50.1174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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