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 46826U 26145.27717564 +.00000000 +00000-0 +00000-0 0 00006
2 46826 53.9825 211.7077 0072503 206.6669 113.0792 2.00564923 01
| Epoch (UTC): | 25 May 2026 06:39:07 |
| Eccentricity: | 0.0072503 |
| inclination: | 53.9825° |
| perigee height: | 19990 km |
| apogee height: | 20375 km |
| right ascension of ascending node: | 211.7077° |
| argument of perigee: | 206.6669° |
| revolutions per day: | 2.00564923 |
| mean anomaly at epoch: | 113.0792° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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