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 45735U 26145.26491334 +.00000000 +00000-0 +39960-3 0 00007
2 45735 53.0441 134.0147 0003151 77.2404 282.8957 15.52705932 07
| Epoch (UTC): | 25 May 2026 06:21:28 |
| Eccentricity: | 0.0003151 |
| inclination: | 53.0441° |
| perigee height: | 407 km |
| apogee height: | 411 km |
| right ascension of ascending node: | 134.0147° |
| argument of perigee: | 77.2404° |
| revolutions per day: | 15.52705932 |
| mean anomaly at epoch: | 282.8957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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