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 54654U 26145.57705193 +.00000000 +00000-0 -72461-4 0 00007
2 54654 87.9265 248.4654 0001639 105.3149 254.8166 13.21827464 08
| Epoch (UTC): | 25 May 2026 13:50:57 |
| Eccentricity: | 0.0001639 |
| inclination: | 87.9265° |
| perigee height: | 1177 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4654° |
| argument of perigee: | 105.3149° |
| revolutions per day: | 13.21827464 |
| mean anomaly at epoch: | 254.8166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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