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 55594U 26145.11229956 +.00000000 +00000-0 +16811-4 0 00005
2 55594 43.0034 293.3506 0001213 269.8190 90.2523 15.27577618 04
| Epoch (UTC): | 25 May 2026 02:41:42 |
| Eccentricity: | 0.0001213 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.3506° |
| argument of perigee: | 269.8190° |
| revolutions per day: | 15.27577618 |
| mean anomaly at epoch: | 90.2523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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