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 55608U 26145.42911343 +.00000000 +00000-0 +90225-5 0 00005
2 55608 43.0052 281.0135 0002162 283.2751 76.7860 15.27575929 05
| Epoch (UTC): | 25 May 2026 10:17:55 |
| Eccentricity: | 0.0002162 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 281.0135° |
| argument of perigee: | 283.2751° |
| revolutions per day: | 15.27575929 |
| mean anomaly at epoch: | 76.7860° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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