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 54669U 26145.58041426 +.00000000 +00000-0 -32950-4 0 00005
2 54669 87.9253 248.4849 0002594 104.7232 255.4190 13.21824581 05
| Epoch (UTC): | 25 May 2026 13:55:47 |
| Eccentricity: | 0.0002594 |
| inclination: | 87.9253° |
| perigee height: | 1176 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 248.4849° |
| argument of perigee: | 104.7232° |
| revolutions per day: | 13.21824581 |
| mean anomaly at epoch: | 255.4190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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