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 51884U 26145.35076933 +.00000000 +00000-0 +29512-4 0 00006
2 51884 53.2137 14.9745 0001439 108.0465 252.0684 15.08838269 07
| Epoch (UTC): | 25 May 2026 08:25:06 |
| Eccentricity: | 0.0001439 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 14.9745° |
| argument of perigee: | 108.0465° |
| revolutions per day: | 15.08838269 |
| mean anomaly at epoch: | 252.0684° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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