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 62186U 26145.63298808 +.00000000 +00000-0 +12130-3 0 00008
2 62186 50.0051 51.4630 0012658 6.8654 353.2395 13.41498558 04
| Epoch (UTC): | 25 May 2026 15:11:30 |
| Eccentricity: | 0.0012658 |
| inclination: | 50.0051° |
| perigee height: | 1094 km |
| apogee height: | 1113 km |
| right ascension of ascending node: | 51.4630° |
| argument of perigee: | 6.8654° |
| revolutions per day: | 13.41498558 |
| mean anomaly at epoch: | 353.2395° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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