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 54184U 26145.07346749 +.00000000 +00000-0 -23552-4 0 00005
2 54184 53.2148 21.5811 0001269 86.9354 273.1783 15.08849141 00
| Epoch (UTC): | 25 May 2026 01:45:47 |
| Eccentricity: | 0.0001269 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 21.5811° |
| argument of perigee: | 86.9354° |
| revolutions per day: | 15.08849141 |
| mean anomaly at epoch: | 273.1783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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