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 54783U 26145.42161020 +.00000000 +00000-0 +33221-4 0 00009
2 54783 53.2129 44.6410 0001454 74.9956 285.1197 15.08836226 08
| Epoch (UTC): | 25 May 2026 10:07:07 |
| Eccentricity: | 0.0001454 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 44.6410° |
| argument of perigee: | 74.9956° |
| revolutions per day: | 15.08836226 |
| mean anomaly at epoch: | 285.1197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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