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 59718U 26144.76588455 +.00000000 +00000-0 +69871-5 0 00004
2 59718 53.1582 311.0356 0000620 74.9450 285.1637 15.69709098 08
| Epoch (UTC): | 24 May 2026 18:22:52 |
| Eccentricity: | 0.0000620 |
| inclination: | 53.1582° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 311.0356° |
| argument of perigee: | 74.9450° |
| revolutions per day: | 15.69709098 |
| mean anomaly at epoch: | 285.1637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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