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 26145.54658603 +.00000000 +00000-0 +00000-0 0 00008
2 39206 4.9511 45.4959 0050247 178.6425 27.7756 1.00269328 04
| Epoch (UTC): | 25 May 2026 13:07:05 |
| Eccentricity: | 0.0050247 |
| inclination: | 4.9511° |
| perigee height: | 35575 km |
| apogee height: | 35999 km |
| right ascension of ascending node: | 45.4959° |
| argument of perigee: | 178.6425° |
| revolutions per day: | 1.00269328 |
| mean anomaly at epoch: | 27.7756° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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