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 57760U 26145.09627204 +.00000000 +00000-0 +18883-3 0 00007
2 57760 81.0111 14.8831 0135569 15.6432 344.8885 14.51457287 08
| Epoch (UTC): | 25 May 2026 02:18:37 |
| Eccentricity: | 0.0135569 |
| inclination: | 81.0111° |
| perigee height: | 625 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 14.8831° |
| argument of perigee: | 15.6432° |
| revolutions per day: | 14.51457287 |
| mean anomaly at epoch: | 344.8885° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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