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 65787U 26145.00819369 +.00000000 +00000-0 +44970-3 0 00007
2 65787 51.9031 50.6674 0001194 98.1849 261.9249 14.79956818 07
| Epoch (UTC): | 25 May 2026 00:11:47 |
| Eccentricity: | 0.0001194 |
| inclination: | 51.9031° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 50.6674° |
| argument of perigee: | 98.1849° |
| revolutions per day: | 14.79956818 |
| mean anomaly at epoch: | 261.9249° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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