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 11153U 26150.44877822 +.00000000 +00000-0 +00000-0 0 00000
2 11153 9.5340 316.1996 0017271 332.1589 49.5111 0.99811182 08
| Epoch (UTC): | 30 May 2026 10:46:14 |
| Eccentricity: | 0.0017271 |
| inclination: | 9.5340° |
| perigee height: | 35843 km |
| apogee height: | 35989 km |
| right ascension of ascending node: | 316.1996° |
| argument of perigee: | 332.1589° |
| revolutions per day: | 0.99811182 |
| mean anomaly at epoch: | 49.5111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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