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 57767U 26145.66080532 +.00000000 +00000-0 +15312-3 0 00008
2 57767 80.9976 29.0647 0006739 84.9845 275.2080 13.85266909 07
| Epoch (UTC): | 25 May 2026 15:51:33 |
| Eccentricity: | 0.0006739 |
| inclination: | 80.9976° |
| perigee height: | 940 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 29.0647° |
| argument of perigee: | 84.9845° |
| revolutions per day: | 13.85266909 |
| mean anomaly at epoch: | 275.2080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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