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 26069.86693359 +.00000000 +00000-0 +37502-4 0 00002
2 11608 81.2173 355.9307 0053235 201.9164 157.9728 14.06552262 05
| Epoch (UTC): | 10 March 2026 20:48:23 |
| Eccentricity: | 0.0053235 |
| inclination: | 81.2173° |
| perigee height: | 833 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 355.9307° |
| argument of perigee: | 201.9164° |
| revolutions per day: | 14.06552262 |
| mean anomaly at epoch: | 157.9728° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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