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 59170U 26145.58805574 +.00000000 +00000-0 +64037-3 0 00008
2 59170 43.0019 353.1918 0003515 293.8034 66.2449 15.27669373 04
| Epoch (UTC): | 25 May 2026 14:06:48 |
| Eccentricity: | 0.0003515 |
| inclination: | 43.0019° |
| perigee height: | 480 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 353.1918° |
| argument of perigee: | 293.8034° |
| revolutions per day: | 15.27669373 |
| mean anomaly at epoch: | 66.2449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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