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 59719U 26144.87860580 +.00000000 +00000-0 -28211-5 0 00003
2 59719 53.1600 311.0419 0000735 96.4672 263.6429 15.69709175 08
| Epoch (UTC): | 24 May 2026 21:05:11 |
| Eccentricity: | 0.0000735 |
| inclination: | 53.1600° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 311.0419° |
| argument of perigee: | 96.4672° |
| revolutions per day: | 15.69709175 |
| mean anomaly at epoch: | 263.6429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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