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 51641U 26145.42113025 +.00000000 +00000-0 -16274-2 0 00009
2 51641 87.8848 40.8133 0001881 77.5330 282.6007 13.10370139 07
| Epoch (UTC): | 25 May 2026 10:06:25 |
| Eccentricity: | 0.0001881 |
| inclination: | 87.8848° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8133° |
| argument of perigee: | 77.5330° |
| revolutions per day: | 13.10370139 |
| mean anomaly at epoch: | 282.6007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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