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 53620U 26145.57016824 +.00000000 +00000-0 +65075-5 0 00008
2 53620 53.2130 248.8265 0001234 88.3127 271.8007 15.08837503 01
| Epoch (UTC): | 25 May 2026 13:41:02 |
| Eccentricity: | 0.0001234 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 248.8265° |
| argument of perigee: | 88.3127° |
| revolutions per day: | 15.08837503 |
| mean anomaly at epoch: | 271.8007° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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