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 11353U 26150.57103808 +.00000000 +00000-0 +00000-0 0 00002
2 11353 7.7602 302.7050 0016829 84.5121 267.1608 0.98544765 09
| Epoch (UTC): | 30 May 2026 13:42:17 |
| Eccentricity: | 0.0016829 |
| inclination: | 7.7602° |
| perigee height: | 36206 km |
| apogee height: | 36350 km |
| right ascension of ascending node: | 302.7050° |
| argument of perigee: | 84.5121° |
| revolutions per day: | 0.98544765 |
| mean anomaly at epoch: | 267.1608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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