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 65124U 26145.65141142 +.00000000 +00000-0 +19559-3 0 00005
2 65124 49.9848 278.6232 0018630 313.1920 46.7461 14.83918704 02
| Epoch (UTC): | 25 May 2026 15:38:01 |
| Eccentricity: | 0.0018630 |
| inclination: | 49.9848° |
| perigee height: | 604 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 278.6232° |
| argument of perigee: | 313.1920° |
| revolutions per day: | 14.83918704 |
| mean anomaly at epoch: | 46.7461° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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