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 57769U 26145.61257473 +.00000000 +00000-0 +17228-4 0 00004
2 57769 81.0052 29.4751 0007181 71.2267 288.9668 13.85463800 07
| Epoch (UTC): | 25 May 2026 14:42:06 |
| Eccentricity: | 0.0007181 |
| inclination: | 81.0052° |
| perigee height: | 939 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 29.4751° |
| argument of perigee: | 71.2267° |
| revolutions per day: | 13.85463800 |
| mean anomaly at epoch: | 288.9668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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