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 39034U 26145.59421514 +.00000000 +00000-0 +00000-0 0 00001
2 39034 0.0675 358.4919 0003798 71.5666 79.8066 1.00274037 06
| Epoch (UTC): | 25 May 2026 14:15:40 |
| Eccentricity: | 0.0003798 |
| inclination: | 0.0675° |
| perigee height: | 35770 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 358.4919° |
| argument of perigee: | 71.5666° |
| revolutions per day: | 1.00274037 |
| mean anomaly at epoch: | 79.8066° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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