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 60019U 26145.50721678 +.00000000 +00000-0 -14059-3 0 00006
2 60019 53.1603 78.8811 0001080 56.5531 303.5572 15.30214694 03
| Epoch (UTC): | 25 May 2026 12:10:23 |
| Eccentricity: | 0.0001080 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 78.8811° |
| argument of perigee: | 56.5531° |
| revolutions per day: | 15.30214694 |
| mean anomaly at epoch: | 303.5572° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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