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 54174U 26145.20445961 +.00000000 +00000-0 +36216-4 0 00005
2 54174 53.2128 325.3736 0001516 92.1047 268.0119 15.08835443 07
| Epoch (UTC): | 25 May 2026 04:54:25 |
| Eccentricity: | 0.0001516 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 325.3736° |
| argument of perigee: | 92.1047° |
| revolutions per day: | 15.08835443 |
| mean anomaly at epoch: | 268.0119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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