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 45061U 26145.11965189 +.00000000 +00000-0 +15064-2 0 00005
2 45061 53.1573 284.2951 0003022 264.5291 95.5368 15.36792623 09
| Epoch (UTC): | 25 May 2026 02:52:17 |
| Eccentricity: | 0.0003022 |
| inclination: | 53.1573° |
| perigee height: | 454 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 284.2951° |
| argument of perigee: | 264.5291° |
| revolutions per day: | 15.36792623 |
| mean anomaly at epoch: | 95.5368° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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