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 18025U 26146.09388282 +.00000000 +00000-0 +63792-3 0 00008
2 18025 63.2918 55.0748 0781802 103.0193 265.9255 13.90150057 04
| Epoch (UTC): | 26 May 2026 02:15:11 |
| Eccentricity: | 0.0781802 |
| inclination: | 63.2918° |
| perigee height: | 357 km |
| apogee height: | 1499 km |
| right ascension of ascending node: | 55.0748° |
| argument of perigee: | 103.0193° |
| revolutions per day: | 13.90150057 |
| mean anomaly at epoch: | 265.9255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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