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 59298U 26145.44707481 +.00000000 +00000-0 +43541-4 0 00000
2 59298 43.0013 157.2012 0001301 272.8264 87.2438 15.27578369 05
| Epoch (UTC): | 25 May 2026 10:43:47 |
| Eccentricity: | 0.0001301 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 157.2012° |
| argument of perigee: | 272.8264° |
| revolutions per day: | 15.27578369 |
| mean anomaly at epoch: | 87.2438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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