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 52161U 26145.57831929 +.00000000 +00000-0 +19423-3 0 00002
2 52161 97.2739 237.5268 0003139 278.6120 81.4778 15.52982520 03
| Epoch (UTC): | 25 May 2026 13:52:46 |
| Eccentricity: | 0.0003139 |
| inclination: | 97.2739° |
| perigee height: | 406 km |
| apogee height: | 410 km |
| right ascension of ascending node: | 237.5268° |
| argument of perigee: | 278.6120° |
| revolutions per day: | 15.52982520 |
| mean anomaly at epoch: | 81.4778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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