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 45185U 26145.43256471 +.00000000 +00000-0 +94463-3 0 00005
2 45185 53.1583 42.1406 0002917 117.9013 242.2285 15.33710433 03
| Epoch (UTC): | 25 May 2026 10:22:53 |
| Eccentricity: | 0.0002917 |
| inclination: | 53.1583° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 42.1406° |
| argument of perigee: | 117.9013° |
| revolutions per day: | 15.33710433 |
| mean anomaly at epoch: | 242.2285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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