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 54640U 26145.59652855 +.00000000 +00000-0 +84490-4 0 00004
2 54640 98.2347 83.1577 0003132 81.0995 279.0559 14.57675484 04
| Epoch (UTC): | 25 May 2026 14:19:00 |
| Eccentricity: | 0.0003132 |
| inclination: | 98.2347° |
| perigee height: | 698 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 83.1577° |
| argument of perigee: | 81.0995° |
| revolutions per day: | 14.57675484 |
| mean anomaly at epoch: | 279.0559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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