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 65525U 26145.43358911 +.00000000 +00000-0 +27493-3 0 00006
2 65525 97.4483 214.9946 0001784 152.3973 207.7349 15.05651463 03
| Epoch (UTC): | 25 May 2026 10:24:22 |
| Eccentricity: | 0.0001784 |
| inclination: | 97.4483° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.9946° |
| argument of perigee: | 152.3973° |
| revolutions per day: | 15.05651463 |
| mean anomaly at epoch: | 207.7349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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