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 55601U 26145.42781409 +.00000000 +00000-0 +26336-4 0 00007
2 55601 43.0027 292.2667 0001331 269.1265 90.9434 15.27577783 09
| Epoch (UTC): | 25 May 2026 10:16:03 |
| Eccentricity: | 0.0001331 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 292.2667° |
| argument of perigee: | 269.1265° |
| revolutions per day: | 15.27577783 |
| mean anomaly at epoch: | 90.9434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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