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 59244U 26145.48100206 +.00000000 +00000-0 +79999-4 0 00003
2 59244 43.0013 69.5728 0001099 255.8138 104.2591 15.27573586 06
| Epoch (UTC): | 25 May 2026 11:32:38 |
| Eccentricity: | 0.0001099 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.5728° |
| argument of perigee: | 255.8138° |
| revolutions per day: | 15.27573586 |
| mean anomaly at epoch: | 104.2591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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