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 54655U 26145.56359161 +.00000000 +00000-0 -51541-4 0 00003
2 54655 87.9250 248.4831 0002842 96.0870 264.0588 13.21828029 03
| Epoch (UTC): | 25 May 2026 13:31:34 |
| Eccentricity: | 0.0002842 |
| inclination: | 87.9250° |
| perigee height: | 1176 km |
| apogee height: | 1180 km |
| right ascension of ascending node: | 248.4831° |
| argument of perigee: | 96.0870° |
| revolutions per day: | 13.21828029 |
| mean anomaly at epoch: | 264.0588° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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