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 49409U 26145.63138093 +.00000000 +00000-0 -24566-3 0 00007
2 49409 53.2167 243.7168 0000636 35.1906 324.9128 15.08844904 04
| Epoch (UTC): | 25 May 2026 15:09:11 |
| Eccentricity: | 0.0000636 |
| inclination: | 53.2167° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 243.7168° |
| argument of perigee: | 35.1906° |
| revolutions per day: | 15.08844904 |
| mean anomaly at epoch: | 324.9128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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