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 55991U 26145.54448687 +.00000000 +00000-0 +57941-4 0 00006
2 55991 43.0059 342.1417 0001785 254.5163 105.5492 15.27572338 00
| Epoch (UTC): | 25 May 2026 13:04:03 |
| Eccentricity: | 0.0001785 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.1417° |
| argument of perigee: | 254.5163° |
| revolutions per day: | 15.27572338 |
| mean anomaly at epoch: | 105.5492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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