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 53631U 26145.54069338 +.00000000 +00000-0 +38302-4 0 00007
2 53631 53.2142 248.6464 0000792 79.3039 280.8042 15.08837755 03
| Epoch (UTC): | 25 May 2026 12:58:35 |
| Eccentricity: | 0.0000792 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 248.6464° |
| argument of perigee: | 79.3039° |
| revolutions per day: | 15.08837755 |
| mean anomaly at epoch: | 280.8042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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