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 53629U 26145.02551236 +.00000000 +00000-0 +59655-4 0 00004
2 53629 53.2178 251.1111 0000609 232.7288 127.3648 15.08840022 03
| Epoch (UTC): | 25 May 2026 00:36:44 |
| Eccentricity: | 0.0000609 |
| inclination: | 53.2178° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 251.1111° |
| argument of perigee: | 232.7288° |
| revolutions per day: | 15.08840022 |
| mean anomaly at epoch: | 127.3648° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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