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 53621U 26145.58122141 +.00000000 +00000-0 -53153-5 0 00005
2 53621 53.2140 248.8943 0000650 55.7676 304.3377 15.08838402 05
| Epoch (UTC): | 25 May 2026 13:56:57 |
| Eccentricity: | 0.0000650 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 248.8943° |
| argument of perigee: | 55.7676° |
| revolutions per day: | 15.08838402 |
| mean anomaly at epoch: | 304.3377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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