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 53019U 26145.24909856 +.00000000 +00000-0 +99344-4 0 00005
2 53019 53.2178 100.4310 0001632 83.5957 276.5221 15.08846389 01
| Epoch (UTC): | 25 May 2026 05:58:42 |
| Eccentricity: | 0.0001632 |
| inclination: | 53.2178° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.4310° |
| argument of perigee: | 83.5957° |
| revolutions per day: | 15.08846389 |
| mean anomaly at epoch: | 276.5221° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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