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 61852U 26145.53458225 +.00000000 +00000-0 +44841-4 0 00002
2 61852 43.0009 163.7017 0001260 274.2122 85.8585 15.27580300 04
| Epoch (UTC): | 25 May 2026 12:49:47 |
| Eccentricity: | 0.0001260 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 163.7017° |
| argument of perigee: | 274.2122° |
| revolutions per day: | 15.27580300 |
| mean anomaly at epoch: | 85.8585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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