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 59857U 26145.43778852 +.00000000 +00000-0 +23318-3 0 00009
2 59857 42.9991 200.9916 0001020 270.0672 90.0062 15.27605345 09
| Epoch (UTC): | 25 May 2026 10:30:24 |
| Eccentricity: | 0.0001020 |
| inclination: | 42.9991° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 200.9916° |
| argument of perigee: | 270.0672° |
| revolutions per day: | 15.27605345 |
| mean anomaly at epoch: | 90.0062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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