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 39417U 26110.87503685 +.00000000 +00000-0 +27812-3 0 00002
2 39417 97.8132 72.9064 0044650 83.9942 276.6367 15.00700152 06
| Epoch (UTC): | 20 April 2026 21:00:03 |
| Eccentricity: | 0.0044650 |
| inclination: | 97.8132° |
| perigee height: | 534 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 72.9064° |
| argument of perigee: | 83.9942° |
| revolutions per day: | 15.00700152 |
| mean anomaly at epoch: | 276.6367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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