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 53192U 26145.42746115 +.00000000 +00000-0 +31918-4 0 00007
2 53192 97.4509 206.4725 0001674 112.5071 247.6334 15.05651124 06
| Epoch (UTC): | 25 May 2026 10:15:32 |
| Eccentricity: | 0.0001674 |
| inclination: | 97.4509° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.4725° |
| argument of perigee: | 112.5071° |
| revolutions per day: | 15.05651124 |
| mean anomaly at epoch: | 247.6334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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