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 25639U 26150.20364572 +.00000000 +00000-0 +00000-0 0 00001
2 25639 12.0575 9.2003 0001522 279.9117 321.4790 0.99026982 08
| Epoch (UTC): | 30 May 2026 04:53:14 |
| Eccentricity: | 0.0001522 |
| inclination: | 12.0575° |
| perigee height: | 36133 km |
| apogee height: | 36146 km |
| right ascension of ascending node: | 9.2003° |
| argument of perigee: | 279.9117° |
| revolutions per day: | 0.99026982 |
| mean anomaly at epoch: | 321.4790° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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