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 53569U 26145.52050727 +.00000000 +00000-0 -35438-4 0 00005
2 53569 53.2129 69.2365 0001000 122.7365 237.3724 15.08845336 01
| Epoch (UTC): | 25 May 2026 12:29:31 |
| Eccentricity: | 0.0001000 |
| inclination: | 53.2129° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 69.2365° |
| argument of perigee: | 122.7365° |
| revolutions per day: | 15.08845336 |
| mean anomaly at epoch: | 237.3724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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