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 59548U 26145.37147852 +.00000000 +00000-0 +43122-3 0 00004
2 59548 42.9991 270.3078 0001271 293.0811 66.9906 15.27587723 02
| Epoch (UTC): | 25 May 2026 08:54:55 |
| Eccentricity: | 0.0001271 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.3078° |
| argument of perigee: | 293.0811° |
| revolutions per day: | 15.27587723 |
| mean anomaly at epoch: | 66.9906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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