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 65626U 26145.16536759 +.00000000 +00000-0 +13352-2 0 00004
2 65626 53.1603 310.8834 0001931 91.4637 268.6587 15.34393773 03
| Epoch (UTC): | 25 May 2026 03:58:07 |
| Eccentricity: | 0.0001931 |
| inclination: | 53.1603° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 310.8834° |
| argument of perigee: | 91.4637° |
| revolutions per day: | 15.34393773 |
| mean anomaly at epoch: | 268.6587° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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