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 55489U 26145.38351012 +.00000000 +00000-0 +43672-3 0 00000
2 55489 43.0044 266.6918 0001606 260.2855 99.7815 15.27525632 04
| Epoch (UTC): | 25 May 2026 09:12:15 |
| Eccentricity: | 0.0001606 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.6918° |
| argument of perigee: | 260.2855° |
| revolutions per day: | 15.27525632 |
| mean anomaly at epoch: | 99.7815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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