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 54661U 26145.54677878 +.00000000 +00000-0 +17909-3 0 00004
2 54661 87.9260 248.4759 0001837 105.8163 254.3174 13.21825760 09
| Epoch (UTC): | 25 May 2026 13:07:21 |
| Eccentricity: | 0.0001837 |
| inclination: | 87.9260° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4759° |
| argument of perigee: | 105.8163° |
| revolutions per day: | 13.21825760 |
| mean anomaly at epoch: | 254.3174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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