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 61559U 26145.58065590 +.00000000 +00000-0 +19418-3 0 00001
2 61559 88.9838 62.0540 0003698 222.4845 137.6036 13.77902585 05
| Epoch (UTC): | 25 May 2026 13:56:08 |
| Eccentricity: | 0.0003698 |
| inclination: | 88.9838° |
| perigee height: | 969 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 62.0540° |
| argument of perigee: | 222.4845° |
| revolutions per day: | 13.77902585 |
| mean anomaly at epoch: | 137.6036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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