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 54758U 26145.04535027 +.00000000 +00000-0 -13881-3 0 00001
2 54758 53.2135 56.5401 0002064 85.2679 274.8548 15.08847626 05
| Epoch (UTC): | 25 May 2026 01:05:18 |
| Eccentricity: | 0.0002064 |
| inclination: | 53.2135° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 56.5401° |
| argument of perigee: | 85.2679° |
| revolutions per day: | 15.08847626 |
| mean anomaly at epoch: | 274.8548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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