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 57663U 26145.55879579 +.00000000 +00000-0 +69336-5 0 00005
2 57663 53.1604 209.9764 0001074 90.1241 269.9883 15.30186514 03
| Epoch (UTC): | 25 May 2026 13:24:39 |
| Eccentricity: | 0.0001074 |
| inclination: | 53.1604° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.9764° |
| argument of perigee: | 90.1241° |
| revolutions per day: | 15.30186514 |
| mean anomaly at epoch: | 269.9883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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