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 53804U 26145.35721800 +.00000000 +00000-0 -19523-5 0 00003
2 53804 53.2131 274.7298 0001046 108.9348 251.1758 15.08838125 00
| Epoch (UTC): | 25 May 2026 08:34:23 |
| Eccentricity: | 0.0001046 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 274.7298° |
| argument of perigee: | 108.9348° |
| revolutions per day: | 15.08838125 |
| mean anomaly at epoch: | 251.1758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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