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 59082U 26145.51655838 +.00000000 +00000-0 +23771-4 0 00000
2 59082 43.0029 236.6206 0002150 253.4890 106.5726 15.27577838 08
| Epoch (UTC): | 25 May 2026 12:23:50 |
| Eccentricity: | 0.0002150 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 236.6206° |
| argument of perigee: | 253.4890° |
| revolutions per day: | 15.27577838 |
| mean anomaly at epoch: | 106.5726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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