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 61886U 26145.25318836 +.00000000 +00000-0 +10769-4 0 00003
2 61886 53.1577 338.5453 0000809 78.2538 281.8570 15.69708731 08
| Epoch (UTC): | 25 May 2026 06:04:35 |
| Eccentricity: | 0.0000809 |
| inclination: | 53.1577° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 338.5453° |
| argument of perigee: | 78.2538° |
| revolutions per day: | 15.69708731 |
| mean anomaly at epoch: | 281.8570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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