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 57864U 26145.22100943 +.00000000 +00000-0 -19377-4 0 00004
2 57864 42.9979 212.8512 0000715 282.0805 77.9966 15.27573927 03
| Epoch (UTC): | 25 May 2026 05:18:15 |
| Eccentricity: | 0.0000715 |
| inclination: | 42.9979° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.8512° |
| argument of perigee: | 282.0805° |
| revolutions per day: | 15.27573927 |
| mean anomaly at epoch: | 77.9966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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