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 59162U 26145.09447766 +.00000000 +00000-0 +58317-4 0 00005
2 59162 43.0046 35.2819 0001756 270.8835 89.1815 15.27588607 03
| Epoch (UTC): | 25 May 2026 02:16:02 |
| Eccentricity: | 0.0001756 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 35.2819° |
| argument of perigee: | 270.8835° |
| revolutions per day: | 15.27588607 |
| mean anomaly at epoch: | 89.1815° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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