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 49424U 26145.52832956 +.00000000 +00000-0 +22660-4 0 00004
2 49424 53.2146 244.1795 0001080 90.9082 269.2033 15.08837265 05
| Epoch (UTC): | 25 May 2026 12:40:47 |
| Eccentricity: | 0.0001080 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 244.1795° |
| argument of perigee: | 90.9082° |
| revolutions per day: | 15.08837265 |
| mean anomaly at epoch: | 269.2033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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