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 45235U 26145.11796865 +.00000000 +00000-0 +11463-2 0 00000
2 45235 53.1569 43.6109 0003054 132.5155 227.6106 15.33725466 03
| Epoch (UTC): | 25 May 2026 02:49:52 |
| Eccentricity: | 0.0003054 |
| inclination: | 53.1569° |
| perigee height: | 463 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 43.6109° |
| argument of perigee: | 132.5155° |
| revolutions per day: | 15.33725466 |
| mean anomaly at epoch: | 227.6106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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