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 49756U 26145.39298052 +.00000000 +00000-0 +10361-2 0 00003
2 49756 53.2134 154.7850 0001270 37.5281 322.5799 15.08966425 00
| Epoch (UTC): | 25 May 2026 09:25:53 |
| Eccentricity: | 0.0001270 |
| inclination: | 53.2134° |
| perigee height: | 538 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 154.7850° |
| argument of perigee: | 37.5281° |
| revolutions per day: | 15.08966425 |
| mean anomaly at epoch: | 322.5799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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