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 26100.02841934 +.00000000 +00000-0 +85534-4 0 00008
2 11608 81.2139 326.6455 0054907 118.2146 242.4582 14.06558743 01
| Epoch (UTC): | 10 April 2026 00:40:55 |
| Eccentricity: | 0.0054907 |
| inclination: | 81.2139° |
| perigee height: | 831 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 326.6455° |
| argument of perigee: | 118.2146° |
| revolutions per day: | 14.06558743 |
| mean anomaly at epoch: | 242.4582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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