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 49759U 26145.45565191 +.00000000 +00000-0 -11424-4 0 00008
2 49759 53.2132 154.5037 0001154 96.7991 263.3133 15.08833261 07
| Epoch (UTC): | 25 May 2026 10:56:08 |
| Eccentricity: | 0.0001154 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.5037° |
| argument of perigee: | 96.7991° |
| revolutions per day: | 15.08833261 |
| mean anomaly at epoch: | 263.3133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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