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 51811U 26145.00300714 +.00000000 +00000-0 -32322-5 0 00000
2 51811 53.2167 356.5359 0001633 83.6707 276.4471 15.08838118 06
| Epoch (UTC): | 25 May 2026 00:04:19 |
| Eccentricity: | 0.0001633 |
| inclination: | 53.2167° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 356.5359° |
| argument of perigee: | 83.6707° |
| revolutions per day: | 15.08838118 |
| mean anomaly at epoch: | 276.4471° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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