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 41773U 26145.02430999 +.00000000 +00000-0 +26985-3 0 00002
2 41773 97.0185 167.9998 0005080 119.8267 240.3486 15.41468443 07
| Epoch (UTC): | 25 May 2026 00:35:00 |
| Eccentricity: | 0.0005080 |
| inclination: | 97.0185° |
| perigee height: | 438 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 167.9998° |
| argument of perigee: | 119.8267° |
| revolutions per day: | 15.41468443 |
| mean anomaly at epoch: | 240.3486° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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