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 45426U 26145.37139319 +.00000000 +00000-0 -36853-3 0 00007
2 45426 87.8917 25.6049 0001479 77.7917 282.3377 13.11415063 05
| Epoch (UTC): | 25 May 2026 08:54:48 |
| Eccentricity: | 0.0001479 |
| inclination: | 87.8917° |
| perigee height: | 1217 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6049° |
| argument of perigee: | 77.7917° |
| revolutions per day: | 13.11415063 |
| mean anomaly at epoch: | 282.3377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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