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 39727U 26145.31734316 +.00000000 +00000-0 +00000-0 0 00007
2 39727 5.0792 69.9778 0002147 13.5599 8.3769 1.00272026 08
| Epoch (UTC): | 25 May 2026 07:36:58 |
| Eccentricity: | 0.0002147 |
| inclination: | 5.0792° |
| perigee height: | 35777 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 69.9778° |
| argument of perigee: | 13.5599° |
| revolutions per day: | 1.00272026 |
| mean anomaly at epoch: | 8.3769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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