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 10669U 26150.55113683 +.00000000 +00000-0 +00000-0 0 00001
2 10669 7.1540 291.6214 0006371 264.7641 87.1603 0.99005265 04
| Epoch (UTC): | 30 May 2026 13:13:38 |
| Eccentricity: | 0.0006371 |
| inclination: | 7.1540° |
| perigee height: | 36118 km |
| apogee height: | 36173 km |
| right ascension of ascending node: | 291.6214° |
| argument of perigee: | 264.7641° |
| revolutions per day: | 0.99005265 |
| mean anomaly at epoch: | 87.1603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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