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 61706U 26145.46209956 +.00000000 +00000-0 -22158-4 0 00005
2 61706 53.1598 157.4853 0001001 90.4147 269.6970 15.34383745 05
| Epoch (UTC): | 25 May 2026 11:05:25 |
| Eccentricity: | 0.0001001 |
| inclination: | 53.1598° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 157.4853° |
| argument of perigee: | 90.4147° |
| revolutions per day: | 15.34383745 |
| mean anomaly at epoch: | 269.6970° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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