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 57766U 26145.66104573 +.00000000 +00000-0 +90401-4 0 00002
2 57766 81.0042 29.1112 0007480 66.1890 294.0050 13.85602739 07
| Epoch (UTC): | 25 May 2026 15:51:54 |
| Eccentricity: | 0.0007480 |
| inclination: | 81.0042° |
| perigee height: | 939 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 29.1112° |
| argument of perigee: | 66.1890° |
| revolutions per day: | 13.85602739 |
| mean anomaly at epoch: | 294.0050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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