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 55585U 26145.37400981 +.00000000 +00000-0 +27877-4 0 00006
2 55585 43.0048 281.4736 0002557 283.8583 76.1984 15.27576705 06
| Epoch (UTC): | 25 May 2026 08:58:34 |
| Eccentricity: | 0.0002557 |
| inclination: | 43.0048° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 281.4736° |
| argument of perigee: | 283.8583° |
| revolutions per day: | 15.27576705 |
| mean anomaly at epoch: | 76.1984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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