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 53924U 26145.66668980 +.00000000 +00000-0 +14229-1 0 00002
2 53924 53.2201 321.4969 0001480 88.5285 342.2705 15.25401378 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001480 |
| inclination: | 53.2201° |
| perigee height: | 489 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 321.4969° |
| argument of perigee: | 88.5285° |
| revolutions per day: | 15.25401378 |
| mean anomaly at epoch: | 342.2705° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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