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 66039U 26145.41654175 +.00000000 +00000-0 +19492-3 0 00006
2 66039 89.0024 45.4869 0002116 69.3335 290.8043 13.51006547 02
| Epoch (UTC): | 25 May 2026 09:59:49 |
| Eccentricity: | 0.0002116 |
| inclination: | 89.0024° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4869° |
| argument of perigee: | 69.3335° |
| revolutions per day: | 13.51006547 |
| mean anomaly at epoch: | 290.8043° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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