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 53744U 26145.36130325 +.00000000 +00000-0 +20986-4 0 00006
2 53744 53.2133 279.5510 0001133 89.9925 270.1197 15.08837760 03
| Epoch (UTC): | 25 May 2026 08:40:16 |
| Eccentricity: | 0.0001133 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 279.5510° |
| argument of perigee: | 89.9925° |
| revolutions per day: | 15.08837760 |
| mean anomaly at epoch: | 270.1197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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