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 53832U 26145.51956127 +.00000000 +00000-0 +18451-4 0 00001
2 53832 53.2144 318.9678 0001269 87.3465 272.7672 15.08834906 02
| Epoch (UTC): | 25 May 2026 12:28:10 |
| Eccentricity: | 0.0001269 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 318.9678° |
| argument of perigee: | 87.3465° |
| revolutions per day: | 15.08834906 |
| mean anomaly at epoch: | 272.7672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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