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 62059U 26145.16876116 +.00000000 +00000-0 +19495-2 0 00009
2 62059 53.1569 54.3751 0001034 96.4297 263.6839 15.69784834 05
| Epoch (UTC): | 25 May 2026 04:03:00 |
| Eccentricity: | 0.0001034 |
| inclination: | 53.1569° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 54.3751° |
| argument of perigee: | 96.4297° |
| revolutions per day: | 15.69784834 |
| mean anomaly at epoch: | 263.6839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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