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 39206U 26032.49648520 +.00000000 +00000-0 +00000-0 0 00004
2 39206 4.7241 45.2584 0051879 182.4767 254.6549 1.00272324 09
| Epoch (UTC): | 01 February 2026 11:54:56 |
| Eccentricity: | 0.0051879 |
| inclination: | 4.7241° |
| perigee height: | 35568 km |
| apogee height: | 36005 km |
| right ascension of ascending node: | 45.2584° |
| argument of perigee: | 182.4767° |
| revolutions per day: | 1.00272324 |
| mean anomaly at epoch: | 254.6549° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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