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 65444U 26145.55586388 +.00000000 +00000-0 +67835-4 0 00005
2 65444 97.4475 359.7652 0002293 74.5792 285.5688 15.05655353 08
| Epoch (UTC): | 25 May 2026 13:20:26 |
| Eccentricity: | 0.0002293 |
| inclination: | 97.4475° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.7652° |
| argument of perigee: | 74.5792° |
| revolutions per day: | 15.05655353 |
| mean anomaly at epoch: | 285.5688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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