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 55385U 26145.60164449 +.00000000 +00000-0 +85715-4 0 00001
2 55385 43.0018 243.9411 0001990 278.1689 81.8937 15.27564743 08
| Epoch (UTC): | 25 May 2026 14:26:22 |
| Eccentricity: | 0.0001990 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.9411° |
| argument of perigee: | 278.1689° |
| revolutions per day: | 15.27564743 |
| mean anomaly at epoch: | 81.8937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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