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 25134U 26086.57603501 +.00000000 +00000-0 +00000-0 0 00007
2 25134 12.7573 11.2846 0002506 208.1963 44.8946 0.99150896 08
| Epoch (UTC): | 27 March 2026 13:49:29 |
| Eccentricity: | 0.0002506 |
| inclination: | 12.7573° |
| perigee height: | 36093 km |
| apogee height: | 36114 km |
| right ascension of ascending node: | 11.2846° |
| argument of perigee: | 208.1963° |
| revolutions per day: | 0.99150896 |
| mean anomaly at epoch: | 44.8946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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