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 49435U 26145.54216850 +.00000000 +00000-0 +26134-3 0 00006
2 49435 53.2149 224.1184 0001231 82.0000 278.1132 15.08849930 01
| Epoch (UTC): | 25 May 2026 13:00:43 |
| Eccentricity: | 0.0001231 |
| inclination: | 53.2149° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.1184° |
| argument of perigee: | 82.0000° |
| revolutions per day: | 15.08849930 |
| mean anomaly at epoch: | 278.1132° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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