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 39509U 26145.51990507 +.00000000 +00000-0 +00000-0 0 00003
2 39509 0.0432 112.2960 0001480 313.8452 41.9243 1.00272706 05
| Epoch (UTC): | 25 May 2026 12:28:39 |
| Eccentricity: | 0.0001480 |
| inclination: | 0.0432° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 112.2960° |
| argument of perigee: | 313.8452° |
| revolutions per day: | 1.00272706 |
| mean anomaly at epoch: | 41.9243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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