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 59544U 26145.39588830 +.00000000 +00000-0 +24383-4 0 00006
2 59544 43.0027 270.4973 0000998 274.7097 85.3641 15.27582833 00
| Epoch (UTC): | 25 May 2026 09:30:04 |
| Eccentricity: | 0.0000998 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.4973° |
| argument of perigee: | 274.7097° |
| revolutions per day: | 15.27582833 |
| mean anomaly at epoch: | 85.3641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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