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 62161U 26145.53515868 +.00000000 +00000-0 +72135-3 0 00009
2 62161 43.0025 87.4843 0000571 275.0701 85.0085 15.27590636 01
| Epoch (UTC): | 25 May 2026 12:50:37 |
| Eccentricity: | 0.0000571 |
| inclination: | 43.0025° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 87.4843° |
| argument of perigee: | 275.0701° |
| revolutions per day: | 15.27590636 |
| mean anomaly at epoch: | 85.0085° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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