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 59782U 26139.77582995 +.00000000 +00000-0 +72874-4 0 00009
2 59782 43.0026 164.2358 0001328 269.6063 90.4636 15.27565105 08
| Epoch (UTC): | 19 May 2026 18:37:11 |
| Eccentricity: | 0.0001328 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.2358° |
| argument of perigee: | 269.6063° |
| revolutions per day: | 15.27565105 |
| mean anomaly at epoch: | 90.4636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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