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 53624U 26145.56279852 +.00000000 +00000-0 +12615-4 0 00004
2 53624 53.2140 248.7804 0001264 90.9482 269.1655 15.08836924 05
| Epoch (UTC): | 25 May 2026 13:30:25 |
| Eccentricity: | 0.0001264 |
| inclination: | 53.2140° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 248.7804° |
| argument of perigee: | 90.9482° |
| revolutions per day: | 15.08836924 |
| mean anomaly at epoch: | 269.1655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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