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 55598U 26145.42782095 +.00000000 +00000-0 +19727-4 0 00000
2 55598 43.0068 280.9890 0003353 283.6631 76.3847 15.27576239 06
| Epoch (UTC): | 25 May 2026 10:16:03 |
| Eccentricity: | 0.0003353 |
| inclination: | 43.0068° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 280.9890° |
| argument of perigee: | 283.6631° |
| revolutions per day: | 15.27576239 |
| mean anomaly at epoch: | 76.3847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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