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 60124U 26145.44551626 +.00000000 +00000-0 -78738-5 0 00006
2 60124 53.1584 203.2506 0001150 71.5780 288.5363 15.69706114 09
| Epoch (UTC): | 25 May 2026 10:41:32 |
| Eccentricity: | 0.0001150 |
| inclination: | 53.1584° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 203.2506° |
| argument of perigee: | 71.5780° |
| revolutions per day: | 15.69706114 |
| mean anomaly at epoch: | 288.5363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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