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 57669U 26145.55831867 +.00000000 +00000-0 +26431-4 0 00007
2 57669 53.1596 209.6783 0001134 94.0365 266.0766 15.31700954 03
| Epoch (UTC): | 25 May 2026 13:23:58 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 209.6783° |
| argument of perigee: | 94.0365° |
| revolutions per day: | 15.31700954 |
| mean anomaly at epoch: | 266.0766° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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