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 51123U 26145.42345353 +.00000000 +00000-0 -21327-5 0 00003
2 51123 53.2117 304.6484 0001330 86.1727 273.9418 15.08835238 07
| Epoch (UTC): | 25 May 2026 10:09:46 |
| Eccentricity: | 0.0001330 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.6484° |
| argument of perigee: | 86.1727° |
| revolutions per day: | 15.08835238 |
| mean anomaly at epoch: | 273.9418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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