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 49762U 26145.41518671 +.00000000 +00000-0 -63868-4 0 00008
2 49762 53.2127 154.6861 0001356 77.3225 282.7918 15.08823278 03
| Epoch (UTC): | 25 May 2026 09:57:52 |
| Eccentricity: | 0.0001356 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.6861° |
| argument of perigee: | 77.3225° |
| revolutions per day: | 15.08823278 |
| mean anomaly at epoch: | 282.7918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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