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 65767U 26145.47009664 +.00000000 +00000-0 +20131-3 0 00008
2 65767 51.9014 58.5807 0000751 102.4048 257.6999 14.79936632 05
| Epoch (UTC): | 25 May 2026 11:16:56 |
| Eccentricity: | 0.0000751 |
| inclination: | 51.9014° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 58.5807° |
| argument of perigee: | 102.4048° |
| revolutions per day: | 14.79936632 |
| mean anomaly at epoch: | 257.6999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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