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 65781U 26145.17700228 +.00000000 +00000-0 +26644-3 0 00000
2 65781 51.9012 49.8774 0000900 100.4937 259.6126 14.79938939 02
| Epoch (UTC): | 25 May 2026 04:14:52 |
| Eccentricity: | 0.0000900 |
| inclination: | 51.9012° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 49.8774° |
| argument of perigee: | 100.4937° |
| revolutions per day: | 14.79938939 |
| mean anomaly at epoch: | 259.6126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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