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 26140.55588181 +.00000000 +00000-0 +00000-0 0 00007
2 39206 4.9413 45.4875 0050560 179.0775 25.7950 1.00275081 00
| Epoch (UTC): | 20 May 2026 13:20:28 |
| Eccentricity: | 0.0050560 |
| inclination: | 4.9413° |
| perigee height: | 35572 km |
| apogee height: | 35999 km |
| right ascension of ascending node: | 45.4875° |
| argument of perigee: | 179.0775° |
| revolutions per day: | 1.00275081 |
| mean anomaly at epoch: | 25.7950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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