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 51128U 26145.50716279 +.00000000 +00000-0 +17631-3 0 00006
2 51128 53.2131 314.2739 0001238 100.9484 259.1647 15.08857831 03
| Epoch (UTC): | 25 May 2026 12:10:18 |
| Eccentricity: | 0.0001238 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.2739° |
| argument of perigee: | 100.9484° |
| revolutions per day: | 15.08857831 |
| mean anomaly at epoch: | 259.1647° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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